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Lockheed SR-71 Blackbird Front View
Picture of the Lockheed SR-71 fron the front.
Lockheed SR-71 Blackbird
The Lockheed SR-71 (known unofficially as the Blackbird, and by its crews as the Habu or the sled) was an advanced, long-range, Mach 3 strategic reconnaissance aircraft developed from the Lockheed YF-12A and A-12 aircraft by the Lockheed Skunk Works. The SR-71 line was in service from 1964 to 1998, and it was the world's fastest and highest-flying operational manned aircraft throughout that entire period, an unparalleled achievement in aviation history. The aircraft flew so fast and so high that if the crew detected a surface-to-air missile launch, the standard evasive action was simply to accelerate. Thirteen aircraft are known to have been lost, all from non-combat related reasons.
The SR-71 included many novel and advanced technologies in order to achieve that performance in particular, due to extensive frictional heating from its high speed, almost everything in the aircraft had to be specially produced the airframe was built almost entirely of titanium, as operating temperatures were too high for aluminium. It was also one of the first aircraft to be have been built with a reduced radar cross section however, the aircraft was not completely stealthy, and still had a fairly large radar signature. The chief designer, Kelly Johnson, was the man behind many of its advanced concepts. After his retirement, Ben Rich ran the program.
Lockheed's previous reconnaissance aircraft was the relatively slow U-2, designed for the Central Intelligence Agency (CIA). In late 1957, the CIA approached the defense contractor Lockheed to build an undetectable spy plane. The project, named Archangel, was led by Kelly Johnson, head of Lockheed's Skunk Works unit in Burbank, California. The work on project Archangel began in the second quarter of 1958, with aim of flying higher and faster than the U-2. Of 11 successive designs drafted in a span of 10 months, "A-10" was the front-runner. Despite this, however, its shape made it vulnerable to radar detection. After a meeting with the CIA in March 1959, the design was modified to have a 90% reduction in radar cross-section. The CIA approved a US$96 million contract for Skunk Works to build a dozen spy planes, named "A-12" on 11 February 1960. The 1960 downing of Francis Gary Powers's U-2 underscored its vulnerability and the need for faster reconnaissance aircraft such as the A-12. 
The A-12 first flew at Groom Lake (Area 51), Nevada, on 25 April 1962. Thirteen were built two variants were also developed, including three of the YF-12 interceptor prototype, and two of the M-21 drone carrier. The aircraft was meant to be powered by the Pratt & Whitney J58 engine, but development ran over schedule, and it was equipped instead with the less powerful Pratt & Whitney J75 initially. The J58s were retrofitted as they became available, and became the standard engine for all subsequent aircraft in the series (A-12, YF-12, M-21), as well as the SR-71. The A-12 flew missions over Vietnam and North Korea before its retirement in 1968. The program's cancellation was announced on 28 December 1966,  due both to budget concerns  and because of the forthcoming SR-71, a derivative of the A-12. 
The SR-71 designation is a continuation of the pre-1962 bomber series the last aircraft built using the series was the XB-70 Valkyrie. However, a bomber variant of the Blackbird was briefly given the B-71 designator, which was retained when the type was changed to SR-71. 
During the later stages of its testing, the B-70 was proposed for a reconnaissance/strike role, with an "RS-70" designation. When the A-12 performance potential was clearly found to be much greater, the USAF ordered a variant of the A-12 in December 1962,  which was originally named R-12 by Lockheed. [N 1] This USAF version was longer and heavier than the original A-12 because it had a longer fuselage to hold more fuel. The R-12 also had a larger two-seat cockpit, and reshaped fuselage chines. Reconnaissance equipment included signals intelligence sensors, a side-looking airborne radar, and a photo camera.  The CIA's A-12 was a better photo-reconnaissance platform than the USAF's R-12, since the A-12 flew somewhat higher and faster,  and with only one pilot, it had room to carry a superior camera  and more instruments. 
During the 1964 campaign, Republican presidential nominee Barry Goldwater repeatedly criticized President Lyndon B. Johnson and his administration for falling behind the Soviet Union in developing new weapons. Johnson decided to counter this criticism by revealing the existence of the YF-12A USAF interceptor, which also served as cover for the still-secret A-12  and the USAF reconnaissance model since July 1964. USAF Chief of Staff General Curtis LeMay preferred the SR (Strategic Reconnaissance) designation and wanted the RS-71 to be named SR-71. Before the July speech, LeMay lobbied to modify Johnson's speech to read "SR-71" instead of "RS-71". The media transcript given to the press at the time still had the earlier RS-71 designation in places, creating the story that the president had misread the aircraft's designation.  [N 2] To conceal the A-12's existence, Johnson referred only to the A-11, while revealing the existence of a high speed, high altitude reconnaissance aircraft. 
In 1968, Secretary of Defense Robert McNamara canceled the F-12 interceptor program. The specialized tooling used to manufacture both the YF-12 and the SR-71 was also ordered destroyed.  Production of the SR-71 totaled 32 aircraft with 29 SR-71As, two SR-71Bs, and the single SR-71C. 
The SR-71 was designed for flight at over Mach 3 with a flight crew of two in tandem cockpits, with the pilot in the forward cockpit and the reconnaissance systems officer operating the surveillance systems and equipment from the rear cockpit, and directing navigation on the mission flight path.   The SR-71 was designed to minimize its radar cross-section, an early attempt at stealth design.  Finished aircraft were painted a dark blue, almost black, to increase the emission of internal heat and to act as camouflage against the night sky. The dark color led to the aircraft's nickname "Blackbird".
While the SR-71 carried radar countermeasures to evade interception efforts, its greatest protection was its combination of high altitude and very high speed, which made it almost invulnerable. Along with its low radar cross-section, these qualities gave a very short time for an enemy surface-to-air missile (SAM) site to acquire and track the aircraft on radar. By the time the SAM site could track the SR-71, it was often too late to launch a SAM, and the SR-71 would be out of range before the SAM could catch up to it. If the SAM site could track the SR-71 and fire a SAM in time, the SAM would expend nearly all of the delta-v of its boost and sustainer phases just reaching the SR-71's altitude at this point, out of thrust, it could do little more than follow its ballistic arc. Merely accelerating would typically be enough for an SR-71 to evade a SAM  changes by the pilots in the SR-71's speed, altitude, and heading were also often enough to spoil any radar lock on the plane by SAM sites or enemy fighters.  At sustained speeds of more than Mach 3.2, the plane was faster than the Soviet Union's fastest interceptor, the Mikoyan-Gurevich MiG-25, which also could not reach the SR-71's altitude.  During its service life, no SR-71 was ever shot down. 
Airframe, canopy, and landing gear Edit
On most aircraft, the use of titanium was limited by the costs involved it was generally used only in components exposed to the highest temperatures, such as exhaust fairings and the leading edges of wings. On the SR-71, titanium was used for 85% of the structure, with much of the rest polymer composite materials.  To control costs, Lockheed used a more easily worked titanium alloy which softened at a lower temperature. [N 3] The challenges posed led Lockheed to develop new fabrication methods, which have since been used in the manufacture of other aircraft. Lockheed found that washing welded titanium requires distilled water, as the chlorine present in tap water is corrosive cadmium-plated tools could not be used, as they also caused corrosion.  Metallurgical contamination was another problem at one point, 80% of the delivered titanium for manufacture was rejected on these grounds.  
The high temperatures generated in flight required special design and operating techniques. Major sections of the skin of the inboard wings were corrugated, not smooth. Aerodynamicists initially opposed the concept, disparagingly referring to the aircraft as a Mach 3 variant of the 1920s-era Ford Trimotor, which was known for its corrugated aluminum skin.  The heat would have caused a smooth skin to split or curl, whereas the corrugated skin could expand vertically and horizontally and had increased longitudinal strength.
Fuselage panels were manufactured to fit only loosely with the aircraft on the ground. Proper alignment was achieved as the airframe heated up and expanded several inches.  Because of this, and the lack of a fuel-sealing system that could handle the airframe's expansion at extreme temperatures, the aircraft leaked JP-7 fuel on the ground prior to takeoff. 
The outer windscreen of the cockpit was made of quartz and was fused ultrasonically to the titanium frame.  The temperature of the exterior of the windscreen reached 600 °F (316 °C) during a mission.  Cooling was carried out by cycling fuel behind the titanium surfaces in the chines. On landing, the canopy temperature was over 572 °F (300 °C). 
The red stripes featured on some SR-71s were to prevent maintenance workers from damaging the skin. Near the center of the fuselage, the curved skin was thin and delicate, with no support from the structural ribs, which were spaced several feet apart. 
The Blackbird's tires, manufactured by B.F. Goodrich, contained aluminum and were filled with nitrogen. They cost $2,300 and would generally require replacing within 20 missions. The Blackbird landed at over 170 knots (200 mph 310 km/h) and deployed a drag parachute to stop the chute also acted to reduce stress on the tires. 
Acquisition of titanium Edit
Titanium was in short supply in the United States, so the Skunk Works team was forced to look elsewhere for the metal. Much of the needed material came from the Soviet Union. Colonel Rich Graham, SR-71 pilot, described the acquisition process:
The airplane is 92% titanium inside and out. Back when they were building the airplane the United States didn't have the ore supplies – an ore called rutile ore. It's a very sandy soil and it's only found in very few parts of the world. The major supplier of the ore was the USSR. Working through Third World countries and bogus operations, they were able to get the rutile ore shipped to the United States to build the SR-71. 
Shape and threat avoidance Edit
The second operational aircraft  designed around a stealth aircraft shape and materials, after the Lockheed A-12,  the SR-71 had several features designed to reduce its radar signature. The SR-71 had a radar cross-section (RCS) around 110 sq ft (10 m 2 ).  Drawing on early studies in radar stealth technology, which indicated that a shape with flattened, tapering sides would reflect most energy away from a radar beam's place of origin, engineers added chines and canted the vertical control surfaces inward. Special radar-absorbing materials were incorporated into sawtooth-shaped sections of the aircraft's skin. Cesium-based fuel additives were used to somewhat reduce exhaust plumes visibility to radar, although exhaust streams remained quite apparent. Kelly Johnson later conceded that Soviet radar technology advanced faster than the stealth technology employed against it. 
The SR-71 featured chines, a pair of sharp edges leading aft from either side of the nose along the fuselage. These were not a feature on the early A-3 design Frank Rodgers, a doctor at the Scientific Engineering Institute, a CIA front organization, discovered that a cross-section of a sphere had a greatly reduced radar reflection, and adapted a cylindrical-shaped fuselage by stretching out the sides of the fuselage.  After the advisory panel provisionally selected Convair's FISH design over the A-3 on the basis of RCS, Lockheed adopted chines for its A-4 through A-6 designs. 
Aerodynamicists discovered that the chines generated powerful vortices and created additional lift, leading to unexpected aerodynamic performance improvements.  The angle of incidence of the delta wings could be reduced for greater stability and less drag at high speeds, and more weight carried, such as fuel. Landing speeds were also reduced, as the chines' vortices created turbulent flow over the wings at high angles of attack, making it harder to stall. The chines also acted like leading-edge extensions, which increase the agility of fighters such as the F-5, F-16, F/A-18, MiG-29, and Su-27. The addition of chines also allowed the removal of the planned canard foreplanes. [N 4]  
Air inlets Edit
The air inlets allowed the SR-71 to cruise at over Mach 3.2, with the air slowing down to subsonic speed as it entered the engine. Mach 3.2 was the design point for the aircraft, its most efficient speed.  However, in practice the SR-71 was sometimes more efficient at even faster speeds—depending on the outside air temperature—as measured by pounds of fuel burned per nautical mile traveled. During one mission, SR-71 pilot Brian Shul flew faster than usual to avoid multiple interception attempts afterward, it was discovered that this had reduced fuel consumption. 
At the front of each inlet, a pointed, movable cone called a "spike" (inlet cone) was locked in its full forward position on the ground and during subsonic flight. When the aircraft accelerated past Mach 1.6, an internal jackscrew moved the spike up to 26 in (66 cm) inwards,  directed by an analog air inlet computer that took into account pitot-static system, pitch, roll, yaw, and angle of attack. Moving the spike tip drew the shock wave riding on it closer to the inlet cowling until it touched just slightly inside the cowling lip. This position reflected the spike shock wave repeatedly between the spike center body and the inlet inner cowl sides, and minimized airflow spillage which is the cause of spillage drag. The air slowed supersonically with a final plane shock wave at entry to the subsonic diffuser. 
Downstream of this normal shock, the air is subsonic. It decelerates further in the divergent duct to give the required speed at entry to the compressor. Capture of the plane's shock wave within the inlet is called "starting the inlet". Bleed tubes and bypass doors were designed into the inlet and engine nacelles to handle some of this pressure and to position the final shock to allow the inlet to remain "started".
In the early years of operation, the analog computers would not always keep up with rapidly changing flight environmental inputs. If internal pressures became too great and the spike was incorrectly positioned, the shock wave would suddenly blow out the front of the inlet, called an "inlet unstart". During unstarts, afterburner extinctions were common. The remaining engine's asymmetrical thrust would cause the aircraft to yaw violently to one side. SAS, autopilot, and manual control inputs would fight the yawing, but often the extreme off-angle would reduce airflow in the opposite engine and stimulate "sympathetic stalls". This generated a rapid counter-yawing, often coupled with loud "banging" noises, and a rough ride during which crews' helmets would sometimes strike their cockpit canopies.  One response to a single unstart was unstarting both inlets to prevent yawing, then restarting them both.  After wind tunnel testing and computer modeling by NASA Dryden test center,  Lockheed installed an electronic control to detect unstart conditions and perform this reset action without pilot intervention.  During troubleshooting of the unstart issue, NASA also discovered the vortices from the nose chines were entering the engine and interfering with engine efficiency. NASA developed a computer to control the engine bypass doors which countered this issue and improved efficiency. Beginning in 1980, the analog inlet control system was replaced by a digital system, which reduced unstart instances. 
The SR-71 was powered by two Pratt & Whitney J58 (company designation JT11D-20) axial-flow turbojet engines. The J58 was a considerable innovation of the era, capable of producing a static thrust of 32,500 lbf (145 kN).   The engine was most efficient around Mach 3.2,  the Blackbird's typical cruising speed. At take-off, the afterburner provided 26% of the thrust. This proportion increased progressively with speed until the afterburner provided all the thrust at about Mach 3. 
Air was initially compressed (and heated) by the inlet spike and subsequent converging duct between the center body and inlet cowl. The shock waves generated slowed the air to subsonic speeds relative to the engine. The air then entered the engine compressor. Some of this compressor flow (20% at cruise) was removed after the fourth compressor stage and went straight to the afterburner through six bypass tubes. Air passing through the turbojet was compressed further by the remaining five compressor stages and then fuel was added in the combustion chamber. After passing through the turbine, the exhaust, together with the compressor bleed air, entered the afterburner. 
At around Mach 3, the temperature rise from the intake compression, added to the engine compressor temperature rise, reduced the allowable fuel flow because the turbine temperature limit did not change. The rotating machinery produced less power, but still enough to run at 100% RPM, thus keeping the airflow through the intake constant. The rotating machinery had become a drag item  and the engine thrust at high speeds came from the afterburner temperature rise.  Maximum flight speed was limited by the temperature of the air entering the engine compressor, which was not certified for temperatures above 800 °F (430 °C). 
Originally, the Blackbird's J58 engines were started with the assistance of two Buick Wildcat V8 internal combustion engines, externally mounted on a vehicle referred to as an AG330 "start cart". The start cart was positioned underneath the J58 and the two Buick engines powered a single, vertical drive shaft connecting to the J58 engine and spinning it to above 3,200 RPM, at which point the turbojet could self-sustain. Once the first J58 engine was started, the cart was repositioned to start the aircraft's other J58 engine. Later start carts used Chevrolet big-block V8 engines. Eventually, a quieter, pneumatic start system was developed for use at main operating bases. The V8 start carts remained at diversion landing sites not equipped with the pneumatic system.  
Several exotic fuels were investigated for the Blackbird. Development began on a coal slurry power plant, but Johnson determined that the coal particles damaged important engine components.  Research was conducted on a liquid hydrogen powerplant, but the tanks for storing cryogenic hydrogen were not of a suitable size or shape.  In practice, the Blackbird would burn somewhat conventional JP-7, which was difficult to light. To start the engines, triethylborane (TEB), which ignites on contact with air, was injected to produce temperatures high enough to ignite the JP-7. The TEB produced a characteristic green flame, which could often be seen during engine ignition. 
On a typical SR-71 mission, the airplane took off with only a partial fuel load to reduce stress on the brakes and tires during takeoff and also ensure it could successfully take off should one engine fail. As a result, the SR-71s were typically refueled immediately after takeoff.  This has led to the misconception that the plane required immediate refueling after takeoff due to leaking fuel tanks. However, leaks were measured in drips per minute and were not significant compared to the overall capacity.  The SR-71 also required in-flight refueling to replenish fuel during long-duration missions. Supersonic flights generally lasted no more than 90 minutes before the pilot had to find a tanker. 
Specialized KC-135Q tankers were required to refuel the SR-71. The KC-135Q had a modified high-speed boom, which would allow refueling of the Blackbird at nearly the tanker's maximum airspeed with minimum flutter. The tanker also had special fuel systems for moving JP-4 (for the KC-135Q itself) and JP-7 (for the SR-71) between different tanks.  As an aid to the pilot when refueling, the cockpit was fitted with a peripheral vision horizon display. This unusual instrument projected a barely visible artificial horizon line across the top of the entire instrument panel, which gave the pilot subliminal cues on aircraft attitude. 
Astro-inertial navigation system Edit
Nortronics, Northrop Corporation's electronics development division, had developed an astro-inertial guidance system (ANS), which could correct inertial navigation system errors with celestial observations, for the SM-62 Snark missile, and a separate system for the ill-fated AGM-48 Skybolt missile, the latter of which was adapted for the SR-71.  [ verification needed ]
Before takeoff, a primary alignment brought the ANS's inertial components to a high degree of accuracy. In flight, the ANS, which sat behind the reconnaissance systems officer's (RSO's), position, tracked stars through a circular quartz glass window on the upper fuselage.  Its "blue light" source star tracker, which could see stars during both day and night, would continuously track a variety of stars as the aircraft's changing position brought them into view. The system's digital computer ephemeris contained data on a list of stars used for celestial navigation: the list first included 56 stars and was later expanded to 61.  The ANS could supply altitude and position to flight controls and other systems, including the mission data recorder, automatic navigation to preset destination points, automatic pointing and control of cameras and sensors, and optical or SLR sighting of fixed points loaded into the ANS before takeoff. According to Richard Graham, a former SR-71 pilot, the navigation system was good enough to limit drift to 1,000 ft (300 m) off the direction of travel at Mach 3. 
Sensors and payloads Edit
The SR-71 originally included optical/infrared imagery systems side-looking airborne radar (SLAR)  electronic intelligence (ELINT) gathering systems  defensive systems for countering missile and airborne fighters     and recorders for SLAR, ELINT, and maintenance data. The SR-71 carried a Fairchild tracking camera and an infrared camera,  both of which ran during the entire mission.
As the SR-71 had a second cockpit behind the pilot for the RSO, it could not carry the A-12's principal sensor, a single large-focal-length optical camera that sat in the "Q-Bay" behind the A-12's single cockpit. Instead, the SR-71's camera systems could be located either in the fuselage chines or the removable nose/chine section. Wide-area imaging was provided by two of Itek's Operational Objective Cameras, which provided stereo imagery across the width of the flight track, or an Itek Optical Bar Camera, which gave continuous horizon-to-horizon coverage. A closer view of the target area was given by the HYCON Technical Objective Camera (TEOC), which could be directed up to 45° left or right of the centerline.  Initially, the TEOCs could not match the resolution of the A-12's larger camera, but rapid improvements in both the camera and film improved this performance.  
SLAR, built by Goodyear Aerospace, could be carried in the removable nose. In later life, the radar was replaced by Loral's Advanced Synthetic Aperture Radar System (ASARS-1). Both the first SLAR and ASARS-1 were ground-mapping imaging systems, collecting data either in fixed swaths left or right of centerline or from a spot location for higher resolution.  ELINT-gathering systems, called the Electro Magnetic Reconnaissance System, built by AIL could be carried in the chine bays to analyze electronic signal fields being passed through, and were programmed to identify items of interest.  
Over its operational life, the Blackbird carried various electronic countermeasures (ECMs), including warning and active electronic systems built by several ECM companies and called Systems A, A2, A2C, B, C, C2, E, G, H, and M. On a given mission, an aircraft carried several of these frequency/purpose payloads to meet the expected threats. Major Jerry Crew, an RSO, told Air & Space/Smithsonian that he used a jammer to try to confuse surface-to-air missile sites as their crews tracked his airplane, but once his threat-warning receiver told him a missile had been launched, he switched off the jammer to prevent the missile from homing in on its signal.  After landing, information from the SLAR, ELINT gathering systems, and the maintenance data recorder were subjected to postflight ground analysis. In the later years of its operational life, a datalink system could send ASARS-1 and ELINT data from about 2,000 nmi (3,700 km) of track coverage to a suitably equipped ground station. [ citation needed ]
Life support Edit
Flying at 80,000 ft (24,000 m) meant that crews could not use standard masks, which could not provide enough oxygen above 43,000 ft (13,000 m). Specialized protective pressurized suits were produced for crew members by the David Clark Company for the A-12, YF-12, M-21 and SR-71. Furthermore, an emergency ejection at Mach 3.2 would subject crews to temperatures of about 450 °F (230 °C) thus, during a high-altitude ejection scenario, an onboard oxygen supply would keep the suit pressurized during the descent. 
The cockpit could be pressurized to an altitude of 10,000 or 26,000 ft (3,000 or 8,000 m) during flight.  The cabin needed a heavy-duty cooling system, as cruising at Mach 3.2 would heat the aircraft's external surface well beyond 500 °F (260 °C)  and the inside of the windshield to 250 °F (120 °C). An air conditioner used a heat exchanger to dump heat from the cockpit into the fuel prior to combustion.  The same air-conditioning system was also used to keep the front (nose) landing gear bay cool, thereby eliminating the need for the special aluminum-impregnated tires similar to those used on the main landing gear. 
Blackbird pilots and RSOs were provided with food and drink for the long reconnaissance flights. Water bottles had long straws which crewmembers guided into an opening in the helmet by looking in a mirror. Food was contained in sealed containers similar to toothpaste tubes which delivered food to the crewmember's mouth through the helmet opening.  
Main era Edit
The first flight of an SR-71 took place on 22 December 1964, at USAF Plant 42 in Palmdale, California, piloted by Bob Gilliland.   The SR-71 reached a top speed of Mach 3.4 during flight testing,   with pilot Major Brian Shul reporting a speed in excess of Mach 3.5 on an operational sortie while evading a missile over Libya.  The first SR-71 to enter service was delivered to the 4200th (later, 9th) Strategic Reconnaissance Wing at Beale Air Force Base, California, in January 1966. 
SR-71s first arrived at the 9th SRW's Operating Location (OL-8) at Kadena Air Base, Okinawa, Japan on 8 March 1968.  These deployments were code-named "Glowing Heat", while the program as a whole was code-named "Senior Crown". Reconnaissance missions over North Vietnam were code-named "Black Shield" and then renamed "Giant Scale" in late 1968.  On 21 March 1968, Major (later General) Jerome F. O'Malley and Major Edward D. Payne flew the first operational SR-71 sortie in SR-71 serial number 61-7976 from Kadena AFB, Okinawa.  During its career, this aircraft (976) accumulated 2,981 flying hours and flew 942 total sorties (more than any other SR-71), including 257 operational missions, from Beale AFB Palmdale, California Kadena Air Base, Okinawa, Japan and RAF Mildenhall, UK. The aircraft was flown to the National Museum of the United States Air Force near Dayton, Ohio in March 1990.
The USAF could fly each SR-71, on average, once per week, because of the extended turnaround required after mission recovery. Very often an aircraft would return with rivets missing, delaminated panels or other broken parts such as inlets requiring repair or replacement. There were cases of the aircraft not being ready to fly again for a month due to the repairs needed. Rob Vermeland, Lockheed Martin's manager of Advanced Development Program, said in an interview in 2015 that high-tempo operations were not realistic for the SR-71. "If we had one sitting in the hangar here and the crew chief was told there was a mission planned right now, then 19 hours later it would be safely ready to take off." 
From the beginning of the Blackbird's reconnaissance missions over North Vietnam and Laos in 1968, the SR-71s averaged approximately one sortie a week for nearly two years. By 1970, the SR-71s were averaging two sorties per week, and by 1972, they were flying nearly one sortie every day. Two SR-71s were lost during these missions, one in 1970 and the second aircraft in 1972, both due to mechanical malfunctions.   Over the course of its reconnaissance missions during the Vietnam War, the North Vietnamese fired approximately 800 SAMs at SR-71s, none of which managed to score a hit.  Pilots did report that missiles launched without radar guidance and no launch detection, had passed as close as 150 yards (140 m) from the aircraft. 
While deployed at Okinawa, the SR-71s and their aircrew members gained the nickname Habu (as did the A-12s preceding them) after a pit viper indigenous to Japan, which the Okinawans thought the plane resembled. 
Operational highlights for the entire Blackbird family (YF-12, A-12, and SR-71) as of about 1990 included: 
- 3,551 mission sorties flown
- 17,300 total sorties flown
- 11,008 mission flight hours
- 53,490 total flight hours
- 2,752 hours Mach 3 time (missions)
- 11,675 hours Mach 3 time (total)
Only one crew member, Jim Zwayer, a Lockheed flight-test reconnaissance and navigation systems specialist, was killed in a flight accident.  The rest of the crew members ejected safely or evacuated their aircraft on the ground.
European flights Edit
European operations were from RAF Mildenhall, England. There were two routes. One was along the Norwegian west coast and up the Kola Peninsula, which contained several large naval bases belonging to the Soviet Navy's Northern Fleet. Over the years, there were several emergency landings in Norway, four in Bodø and two of them in 1981 (flying from Beale) and 1985. Rescue parties were sent in to repair the planes before leaving. On one occasion, one complete wing with engine was replaced as the easiest way to get the plane airborne again.   The other route, from Mildenhall over the Baltic Sea, was known as the Baltic Express.
Swedish Air Force fighter pilots have managed to lock their radar on an SR-71 on multiple occasions within shooting range.   [ clarification needed ] Target illumination was maintained by feeding target location from ground-based radars to the fire-control computer in the JA 37 Viggen interceptor.  The most common site for the lock-on was the thin stretch of international airspace between Öland and Gotland that the SR-71s used on their return flights.   
On 29 June 1987, an SR-71 was on a mission around the Baltic Sea to spy on Soviet postings when one of the engines exploded. The aircraft, which was at 20 km altitude, quickly lost altitude and turned 180° to the left and turned over Gotland to search for the Swedish coast. Thus, Swedish airspace was violated, whereupon two armed Saab JA 37 Viggens on an exercise at the height of Västervik were ordered there. The mission was to do an incident preparedness check and identify an aircraft of high interest. It was found that the plane was in obvious distress and a decision was made that the Swedish Air Force would escort the plane out of the Baltic Sea. A second round of armed JA-37s from Ängelholm replaced the first pair and completed the escort to Danish airspace. The event had been classified for over 30 years, and when the report was unsealed, data from the NSA showed that a few MiG-25s with the order to shoot down the SR-71 or force it to land, had started right after the engine failure. A MiG-25 had locked a missile on the damaged SR-71, but as the aircraft was under escort, no missiles were fired. On 29 November 2018, the four Swedish pilots involved were awarded medals from the USAF.  
Initial retirement Edit
One view is that the SR-71 program was terminated due to Pentagon politics, and not because the aircraft had become obsolete, irrelevant, suffered maintenance problems, or had unsustainable program costs.  In the 1970s and early 1980s, SR-71 squadron and wing commanders were often promoted into higher positions as general officers within the USAF structure and the Pentagon. (In order to be selected into the SR-71 program in the first place, a pilot or navigator (RSO) had to be a top-quality USAF officer, so continuing career progression for members of this elite group was not surprising.) These generals were adept at communicating the value of the SR-71 to a USAF command staff and a Congress who often lacked a basic understanding of how the SR-71 worked and what it did. However, by the mid-1980s, these SR-71 generals all had retired, and a new generation of USAF generals wanted to cut the program's budget and spend its funding on new strategic bomber programs instead, especially the very expensive B-2 Spirit. 
The USAF may have seen the SR-71 as a bargaining chip to ensure the survival of other priorities. Also, the SR-71 program's "product", which was operational and strategic intelligence, was not seen by these generals as being very valuable to the USAF. The primary consumers of this intelligence were the CIA, NSA, and DIA. A general misunderstanding of the nature of aerial reconnaissance and a lack of knowledge about the SR-71 in particular (due to its secretive development and operations) was used by detractors to discredit the aircraft, with the assurance given that a replacement was under development. Dick Cheney told the Senate Appropriations Committee that the SR-71 cost $85,000 per hour to operate.  Opponents estimated the aircraft's support cost at $400 to $700 million per year, though the cost was actually closer to $300 million. 
The SR-71, while much more capable than the Lockheed U-2 in terms of range, speed, and survivability, suffered the lack of a data link, which the U-2 had been upgraded to carry. This meant that much of the SR-71's imagery and radar data could not be used in real time, but had to wait until the aircraft returned to base. This lack of immediate real-time capability was used as one of the justifications to close down the program. Attempts to add a datalink to the SR-71 were stymied early on by the same factions in the Pentagon and Congress who were already set on the program's demise, even in the early 1980s.  These same factions also forced expensive sensor upgrades to the SR-71, which did little to increase its mission capabilities, but could be used as justification for complaining about the cost of the program. 
In 1988, Congress was convinced to allocate $160,000 to keep six SR-71s and a trainer model in flyable storage that could become flightworthy within 60 days. However, the USAF refused to spend the money. While the SR-71 survived attempts to retire it in 1988, partly due to the unmatched ability to provide high-quality coverage of the Kola Peninsula for the US Navy,  the decision to retire the SR-71 from active duty came in 1989, with the last missions flown in October that year.  Four months after the plane's retirement, General Norman Schwarzkopf Jr., was told that the expedited reconnaissance, which the SR-71 could have provided, was unavailable during Operation Desert Storm. 
The SR-71 program's main operational capabilities came to a close at the end of fiscal year 1989 (October 1989). The 1st Strategic Reconnaissance Squadron (1 SRS) kept its pilots and aircraft operational and active, and flew some operational reconnaissance missions through the end of 1989 and into 1990, due to uncertainty over the timing of the final termination of funding for the program. The squadron finally closed in mid-1990, and the aircraft were distributed to static display locations, with a number kept in reserve storage. 
From the operator's perspective, what I need is something that will not give me just a spot in time but will give me a track of what is happening. When we are trying to find out if the Serbs are taking arms, moving tanks or artillery into Bosnia, we can get a picture of them stacked up on the Serbian side of the bridge. We do not know whether they then went on to move across that bridge. We need the [data] that a tactical, an SR-71, a U-2, or an unmanned vehicle of some sort, will give us, in addition to, not in replacement of, the ability of the satellites to go around and check not only that spot but a lot of other spots around the world for us. It is the integration of strategic and tactical.
Due to unease over political situations in the Middle East and North Korea, the U.S. Congress re-examined the SR-71 beginning in 1993.  Rear Admiral Thomas F. Hall addressed the question of why the SR-71 was retired, saying it was under "the belief that, given the time delay associated with mounting a mission, conducting a reconnaissance, retrieving the data, processing it, and getting it out to a field commander, that you had a problem in timelines that was not going to meet the tactical requirements on the modern battlefield. And the determination was that if one could take advantage of technology and develop a system that could get that data back real time. that would be able to meet the unique requirements of the tactical commander." Hall also stated they were "looking at alternative means of doing [the job of the SR-71]." 
Macke told the committee that they were "flying U-2s, RC-135s, [and] other strategic and tactical assets" to collect information in some areas.  Senator Robert Byrd and other Senators complained that the "better than" successor to the SR-71 had yet to be developed at the cost of the "good enough" serviceable aircraft. They maintained that, in a time of constrained military budgets, designing, building, and testing an aircraft with the same capabilities as the SR-71 would be impossible. 
Congress's disappointment with the lack of a suitable replacement for the Blackbird was cited concerning whether to continue funding imaging sensors on the U-2. Congressional conferees stated the "experience with the SR-71 serves as a reminder of the pitfalls of failing to keep existing systems up-to-date and capable in the hope of acquiring other capabilities."  It was agreed to add $100 million to the budget to return three SR-71s to service, but it was emphasized that this "would not prejudice support for long-endurance UAVs" [such as the Global Hawk]. The funding was later cut to $72.5 million.  The Skunk Works was able to return the aircraft to service under budget at $72 million. 
Retired USAF Colonel Jay Murphy was made the Program Manager for Lockheed's reactivation plans. Retired USAF Colonels Don Emmons and Barry MacKean were put under government contract to remake the plane's logistic and support structure. Still-active USAF pilots and Reconnaissance Systems Officers (RSOs) who had worked with the aircraft were asked to volunteer to fly the reactivated planes. The aircraft was under the command and control of the 9th Reconnaissance Wing at Beale Air Force Base and flew out of a renovated hangar at Edwards Air Force Base. Modifications were made to provide a data-link with "near real-time" transmission of the Advanced Synthetic Aperture Radar's imagery to sites on the ground. 
Final retirement Edit
The reactivation met much resistance: the USAF had not budgeted for the aircraft, and UAV developers worried that their programs would suffer if money was shifted to support the SR-71s. Also, with the allocation requiring yearly reaffirmation by Congress, long-term planning for the SR-71 was difficult.  In 1996, the USAF claimed that specific funding had not been authorized, and moved to ground the program. Congress reauthorized the funds, but, in October 1997, President Bill Clinton attempted to use the line-item veto to cancel the $39 million allocated for the SR-71. In June 1998, the U.S. Supreme Court ruled that the line-item veto was unconstitutional. All this left the SR-71's status uncertain until September 1998, when the USAF called for the funds to be redistributed the USAF permanently retired it in 1998.
NASA operated the two last airworthy Blackbirds until 1999.  All other Blackbirds have been moved to museums except for the two SR-71s and a few D-21 drones retained by the NASA Dryden Flight Research Center (later renamed the Armstrong Flight Research Center). 
- 24 December 1957: First J58 engine run
- 1 May 1960: Francis Gary Powers is shot down in a Lockheed U-2 over the Soviet Union
- 13 June 1962: SR-71 mock-up reviewed by the USAF
- 30 July 1962: J58 completes pre-flight testing
- 28 December 1962: Lockheed signs contract to build six SR-71 aircraft
- 25 July 1964: President Johnson makes public announcement of SR-71
- 29 October 1964: SR-71 prototype (AF Ser. No. 61-7950) delivered to Air Force Plant 42 at Palmdale, California
- 7 December 1964: Beale AFB, CA, announced as base for SR-71
- 22 December 1964: First flight of the SR-71, with Lockheed test pilot Robert J "Bob" Gilliland at Palmdale 
- 21 July 1967: Jim Watkins and Dave Dempster fly first international sortie in SR-71A, AF Ser. No. 61-7972, when the Astro-Inertial Navigation System (ANS) fails on a training mission and they accidentally fly into Mexican airspace
- 5 February 1968: Lockheed ordered to destroy A-12, YF-12, and SR-71 tooling
- 8 March 1968: First SR-71A (AF Ser. No. 61-7978) arrives at Kadena AB, Okinawa to replace A-12s
- 21 March 1968: First SR-71 (AF Ser. No. 61-7976) operational mission flown from Kadena AB over Vietnam
- 29 May 1968: CMSgt Bill Gornik begins the tie-cutting tradition of Habu crews' neckties
- 3 December 1975: First flight of SR-71A (AF Ser. No. 61-7959) in "big tail" configuration
- 20 April 1976: TDY operations started at RAF Mildenhall, United Kingdom with SR-71A, AF Ser. No. 61-7972
- 27–28 July 1976: SR-71A sets speed and altitude records (altitude in horizontal flight: 85,068.997 ft (25,929.030 m) and speed over a straight course: 2,193.167 miles per hour (3,529.560 km/h))
- August 1980: Honeywell starts conversion of AFICS to DAFICS
- 15 January 1982: SR-71B, AF Ser. No. 61-7956, flies its 1,000th sortie
- 21 April 1989: SR-71, AF Ser. No. 61-7974, is lost due to an engine explosion after taking off from Kadena AB, the last Blackbird to be lost 
- 22 November 1989: USAF SR-71 program officially terminated
- 6 March 1990: Last SR-71 flight under Senior Crown program, setting four speed records en route to the Smithsonian Institution
- 25 July 1991: SR-71B, AF Ser. No. 61-7956/NASA No. 831 officially delivered to NASA Dryden Flight Research Center at Edwards AFB, California
- October 1991: NASA engineer Marta Bohn-Meyer becomes the first female SR-71 crew member
- 28 September 1994: Congress votes to allocate $100 million for reactivation of three SR-71s
- 28 June 1995: First reactivated SR-71 returns to USAF as Detachment 2
- 9 October 1999: The last flight of the SR-71 (AF Ser. No. 61-7980/NASA 844)
The SR-71 was the world's fastest and highest-flying air-breathing operational manned aircraft throughout its career. On 28 July 1976, SR-71 serial number 61-7962, piloted by then Captain Robert Helt, broke the world record: an "absolute altitude record" of 85,069 feet (25,929 m).     Several aircraft have exceeded this altitude in zoom climbs, but not in sustained flight.  That same day SR-71 serial number 61-7958 set an absolute speed record of 1,905.81 knots (2,193.2 mph 3,529.6 km/h), approximately Mach 3.3.   SR-71 pilot Brian Shul states in his book The Untouchables that he flew in excess of Mach 3.5 on 15 April 1986 over Libya to evade a missile. 
The SR-71 also holds the "speed over a recognized course" record for flying from New York to London—distance 3,461.53 miles (5,570.79 km), 1,806.964 miles per hour (2,908.027 km/h), and an elapsed time of 1 hour 54 minutes and 56.4 seconds—set on 1 September 1974, while flown by USAF pilot James V. Sullivan and Noel F. Widdifield, reconnaissance systems officer (RSO).  This equates to an average speed of about Mach 2.72, including deceleration for in-flight refueling. Peak speeds during this flight were likely closer to the declassified top speed of over Mach 3.2. For comparison, the best commercial Concorde flight time was 2 hours 52 minutes and the Boeing 747 averages 6 hours 15 minutes.
On 26 April 1971, 61-7968, flown by majors Thomas B. Estes and Dewain C. Vick, flew over 15,000 miles (24,000 km) in 10 hours and 30 minutes. This flight was awarded the 1971 Mackay Trophy for the "most meritorious flight of the year" and the 1972 Harmon Trophy for "most outstanding international achievement in the art/science of aeronautics". 
When the SR-71 was retired in 1990, one Blackbird was flown from its birthplace at USAF Plant 42 in Palmdale, California, to go on exhibit at what is now the Smithsonian Institution's Steven F. Udvar-Hazy Center in Chantilly, Virginia. On 6 March 1990, Lt. Col. Raymond E. Yeilding and Lt. Col. Joseph T. Vida piloted SR-71 S/N 61-7972 on its final Senior Crown flight and set four new speed records in the process:
- Los Angeles, California, to Washington, D.C., distance 2,299.7 miles (3,701.0 km), average speed 2,144.8 miles per hour (3,451.7 km/h), and an elapsed time of 64 minutes 20 seconds.  to East Coast, distance 2,404 miles (3,869 km), average speed 2,124.5 miles per hour (3,419.1 km/h), and an elapsed time of 67 minutes 54 seconds.
- Kansas City, Missouri, to Washington, D.C., distance 942 miles (1,516 km), average speed 2,176 miles per hour (3,502 km/h), and an elapsed time of 25 minutes 59 seconds.
- St. Louis, Missouri, to Cincinnati, Ohio, distance 311.4 miles (501.1 km), average speed 2,189.9 miles per hour (3,524.3 km/h), and an elapsed time of 8 minutes 32 seconds.
These four speed records were accepted by the National Aeronautic Association (NAA), the recognized body for aviation records in the United States.  Additionally, Air & Space/Smithsonian reported that the USAF clocked the SR-71 at one point in its flight reaching 2,242.48 miles per hour (3,608.92 km/h).  After the Los Angeles–Washington flight, on 6 March 1990, Senator John Glenn addressed the United States Senate, chastising the Department of Defense for not using the SR-71 to its full potential:
Mr. President, the termination of the SR-71 was a grave mistake and could place our nation at a serious disadvantage in the event of a future crisis. Yesterday's historic transcontinental flight was a sad memorial to our short-sighted policy in strategic aerial reconnaissance. 
Speculation existed regarding a replacement for the SR-71, including a rumored aircraft codenamed Aurora. The limitations of reconnaissance satellites, which take up to 24 hours to arrive in the proper orbit to photograph a particular target, make them slower to respond to demand than reconnaissance planes. The fly-over orbit of spy satellites may also be predicted and can allow assets to be hidden when the satellite is above, a drawback not shared by aircraft. Thus, there are doubts that the US has abandoned the concept of spy planes to complement reconnaissance satellites.  Unmanned aerial vehicles (UAVs) are also used for much aerial reconnaissance in the 21st century, being able to overfly hostile territory without putting human pilots at risk, as well as being smaller and harder to detect than man-carrying aircraft.
On 1 November 2013, media outlets reported that Skunk Works has been working on an unmanned reconnaissance airplane it has named SR-72, which would fly twice as fast as the SR-71, at Mach 6.   However, the USAF is officially pursuing the Northrop Grumman RQ-180 UAV to take up the SR-71's strategic ISR role. 
Rare photos of the SR-71 Blackbird show its amazing history
The SR-71 Blackbird is, without a doubt, the most advanced airplane ever built in relation to the technology available at the time. It broke all aviation records, it flew incredible missions, and it became the stuff of legend. Lockheed Martin published its history in this collection of high resolution scans of old photos.
The SR-71 was a technological marvel. Practically every area of design required new approaches or breakthroughs in technology. To withstand high temperatures generated by friction in the upper atmosphere during sustained Mach 3 flight, the Blackbird required an array of specially developed materials including high temperature fuel, sealants, lubricants, wiring and other components. Ninety-three percent of the Blackbird's airframe consisted of titanium alloy that allowed the aircraft to operate in a regime where temperatures range from 450 degrees Fahrenheit at its aft midsection to 950 degrees Fahrenheit near the engine exhaust. The cockpit canopy, made of special heat resistant glass, had to withstand surface temperatures as high as 640 degrees Fahrenheit.
Photos and captions courtesy of Lockheed Martin.
The history of the SR-71 in photos
Two of the leading figures in the U-2 program, the CIA's Richard Bissell and Lockheed designer Kelly Johnson, had as early as 1955 decided to explore a follow-on reconnaissance aircraft that would seek to remedy the U-2's unexpected flaw—its easy tracking by Soviet radar.
The Story of Secret SR-91 Aurora hypothesized aircraft design to replace the SR-71 Blackbird
SR-91 Aurora aircraft design was a rumored mid-1980s American reconnaissance aircraft. It is believed that SR-91 Aurora is capable of hypersonic flight at speeds of Mach 5+.
According to the hypothesis, Aurora was developed in the 1980s or 1990s as a replacement for the aging and expensive SR-71 Blackbird.
Aurora also known as SR-91 Aurora is the popular name for a hypothesized American reconnaissance aircraft, believed by some to be capable of hypersonic flight at speeds of Mach 5+.
According to the hypothesis, Aurora was developed in the 1980s or 1990s as a replacement for the aging and expensive SR-71 Blackbird.
Here is a Documentary on SR-91 Aurora – Does it Exists?
Related Article: SR-91 Aurora aircraft – hypersonic reconnaissance aircraft – Mach 5+ fighter jet
The Aurora legend started in March 1990, when Aviation Week & Space Technology magazine broke the news that the term “Aurora” had been inadvertently included in the 1985 U.S. budget, as an allocation of $455 million for “black aircraft production” in FY 1987.
According to Aviation Week, Project Aurora referred to a group of exotic aircraft, and not to one particular airframe. Funding of the project allegedly reached $2.3 billion in fiscal 1987, according to a 1986 procurement document obtained by Aviation Week. In the 1994 book Skunk Works, Ben Rich, the former head of Lockheed’s Skunk Works division, wrote that the Aurora was the budgetary code name for the stealth bomber fly-off that resulted in the B-2 Spirit.
By the mid-1990s reports surfaced of sightings of unidentified aircraft flying over California and the United Kingdom involving odd-shaped contrails, sonic booms, and related phenomena that suggested the US had developed such an aircraft. Nothing ever linked any of these observations to any program or aircraft type, but the name Aurora was often tagged on these as a way of explaining the observations.
An artist’s conception of the Aurora aircraft Via Wikipedia
Related Article: List of Top 15 Secret Military Aircraft projects in history
The well-known instance which provides evidence of such an aircraft’s existence is the sighting of a triangular plane over the North Sea in August 1989 by oil-exploration engineer Chris Gibson.
In another incident of the famous “sky quakes” heard over Los Angeles since the early 1990s, found to be heading for the secret Groom Lake (Area 51) installation in the Nevada desert, numerous other facts provide an understanding of how the aircraft’s technology works. Rumored to exist but routinely denied by U.S. officials, the name of this aircraft is Aurora.
The outside world uses the name Aurora because a censor’s slip let it appear below the SR-71 Blackbird and U-2 in the 1985 Pentagon budget request. Even if this was the actual name of the project, it would have by now been changed after being compromised in such a manner.
The plane’s real name has been kept a secret along with its existence. This is not unfamiliar though, the F-117a stealth fighter was kept a secret for over ten years after its first pre-production test flight.
Related Article: Here’s list of Abandoned and Declassified Black Projects
The project is what is technically known as a Special Access Program (SAP). More often, such projects are referred to as “black programs.”
On 6 March 1990, one of the United States Air Force’s Lockheed SR-71 Blackbird spyplanes shattered the official air speed record from Los Angeles to Washington’s Dulles Airport.
There, a brief ceremony marked the end of the SR-71’s operational career. Officially, the SR-71 was being retired to save the $200-$300 million a year it cost to operate the fleet. Some reporters were told the plane had been made redundant by sophisticated spy satellites.
A British Ministry of Defence report released in May 2006 refers to USAF priority plans to produce a Mach 4-6 highly supersonic vehicle, but no conclusive evidence had emerged to confirm the existence of such a project.
It was believed by some that the Aurora project was canceled due to a shift from spy-planes to high-tech unmanned aerial vehicles and reconnaissance satellites which can do the same job as a spy plane, but with less risk of casualties.
In June 2017, Aviation Week reported that Rob Weiss, the General Manager of the Skunk Works, provided some confirmation of a research project and stated that hypersonic technology was now mature, and efforts were underway to fly an aircraft with it.
Lockheed SR-71 Blackbird
Born out of the need of a high-altitude, high-speed, strategic reconnaissance aircraft, the SR-71 Blackbird is one of the world's most iconic aircraft ever produced. The youngest in the Blackbird Family, the SR-71 was the third aircraft to use the design of it's type. The first was the A-12 Oxcart, which preceded the SR-71 by a few years, followed by the YF-12. The SR-71 was also the smallest of the trio, flying slightly lower and slightly slower than it's predecessors.
The collapse of the Soviet Union coupled with the increase of spy satellite coverage led to it's retirement in 1989, however the USAF pushed for it's restoration in 1994. NASA also took interest in the design, using it for a number of different missions during the late 1980s, and then again from 1994 through about 2006. The introduction of stable and well designed drones also rendered the SR-71 relatively obsolete, however there has been no aircraft to fulfill the mission requirements at it's specification since. Such a gap in mission necessity has resulted in an increase of speculation on it's service status and a successor. As early as 1990, individuals have speculated on the existence of an SR-72 aircraft. Another suspected replacement was called Aurora, but it has been noted that this designation was associated with the B-2 Spirit bomber project. Lockheed has since all but confirmed it's intentions of an SR-72 aircraft as a replacement or stop-gap measure between it's proposed TR-X program and the U-2S.
To this day, the SR-71 retains numerous speed and altitude records from around the world and also remains one of the most well guarded aircraft to have ever existed.
It's mission sets are maintained by the Lockheed MQ-170, Lockheed U-2S, Boeing RC-135, Boeing P-8, and other modified recon-second-mission aircraft.
Blackbird SR-71: Master Of Stealth-The Fastest Airplane Ever Built
While the Lockheed Martin SR-71 Blackbird, flown by the United States Air Force from 1964, was officially retired in 1990 (albeit with a brief return to service from 1995-1998), it established the record for the fastest “air-breathing manned aircraft” in the world back in 1976 and to this day, that record has never been broken.
The Blackbird – as the SR-71 came to be known, due to its entirely matte black exterior – was able to travel at an astonishing 2,199.65 mph (3,540 km/h), and could reach an altitude of 85,000 feet. The Blackbird was thus theoretically able to outrun any enemy aircraft on earth, as well as being able to outrun any SAM (surface-to-air missile) fired at it.
During the entire course of its operational history, no Blackbird was ever lost to enemy action.
SR-71 production at Lockheed Skunk Works.
What is quite amazing about the SR-71 Blackbird is just how incredibly advanced the technology used in its design was for its time.
Design started on the Blackbird in 1958 – a mere thirteen years after the end of WWII – after the CIA approached Lockheed to design and build a spy plane that would be as close to undetectable as possible, and able to replace (and significantly outperform) the Lockheed U-2 spy planes that were used at the time.
After a few years of design and development, the first SR-71 was flown on 22 December 1964.
As a strategic reconnaissance aircraft, stealth and speed were vital to the Blackbird’s design, and it excels in both of these areas. As already stated, it was capable of flying at speeds of over Mach 3.3 (rumored by some, though, to be over Mach 4), a feat unequaled before or since by any other manned aircraft.
With regard to stealth, the Blackbird had a Radar Cross Section (RCS) of a light aircraft, a feat of deception achieved by the incredible design and unusual materials that were used for the plane.
This near-invisibility to enemy radar was made possible by the use of epoxy and asbestos in the Blackbird’s vertical rudders and leading edges, as well as the use of an iron ferrite-based anti-radar coating on the leading edges.
The Lockheed SR-71.Photo: James (Jim) Gordon CC BY 2.0
The rest of the Blackbird’s skin, around 85% of it, was made from titanium and titanium alloy, while the internal airframe was made largely from aluminum. These elements all meant that, all in all, the Blackbird’s RCS was a mere tenth of something like an F-15’s, which meant it would show up – if detected at all – on enemy radar as a minuscule target.
An air-to-air overhead front view of an SR-71A strategic reconnaissance aircraft. The SR-71 is unofficially known as the “Blackbird.”
The materials used to reduce the Blackbird’s RCS also contributed to the plane’s ability to withstand the extremely high temperatures generated by flying at the massive speeds of which it was capable. The matte black coating which covered the entire aircraft also provided visual camouflage against dark skies.
Dryden’s SR-71B Blackbird, NASA 831, slices across the snow-covered southern Sierra Nevada Mountains of California after being refueled by an Air Force tanker during a 1994 flight. SR-71B was the trainer version of the SR-71. The dual cockpit was to allow the instructor to fly.
Because the Blackbird flew at such high altitudes, standard oxygen masks and flight suits would not be adequate for the pilots of the SR-71. Thus, the flight suits designed for and worn by Blackbird pilots had more in common with astronauts’ space suits than anything worn by pilots of other military aircraft.
These suits were extremely necessary owing to the fact that if anything went wrong at 85,000 feet, such as the loss of cabin pressure or the need to eject, death would be almost instantaneous in most other flight suits. Thus a pressure suit, Model 1030, was designed by the David Clark Company specifically for Blackbird pilots.
The crew of a NASA Lockheed SR-71 Blackbird standing by the aircraft in their pressurized flight suits
While no Blackbird was ever shot down by enemy action, that didn’t mean that nobody tried to achieve this. In 1981, on August 26, Reconnaissance Systems Officer Major Ed McKinn and Major Maury Rosenberg were making multiple passes over the demilitarized zone (DMZ) between North Korea and South Korea when they sighted a SAM headed their way.
A self-portrait of Brian Shul in full flight suit gear within the cockpit of the SR-71 Blackbird.
Using the incredible speed of the Blackbird, they were able to evade the missile, which detonated around a mile away for them – which, in terms of how fast this plane could fly, counts as a pretty close shave.
It has been estimated that a couple hundred missiles were fired at Blackbirds over the few decades in which they were operational, but this was about the closest a missile ever came to hitting one.
Lockheed SR-71A Blackbird, cockpit, forward view
With such outstanding – indeed, unmatched – performance as a strategic reconnaissance aircraft, why then was the Blackbird retired permanently from service back in 1998?
One factor was undoubtedly cost: the Blackbird’s design called for extremely specialized maintenance, and the plane used very unique (and expensive) fuel. It has been estimated that with all the costs taken into account, a Blackbird could cost $200,000 per hour to operate.
SR-71 in flight
Another factor in the Blackbird’s retirement was the development of improved reconnaissance satellites, which could be operated much more cheaply and efficiently.
An SR-71 refueling from a KC-135Q Stratotanker during a flight in 1983
Finally, there was internal Pentagon politics and disagreements. All of these factors meant that the world’s fastest plane was permanently retired toward the end of 1998.
The records held by the Blackbird still stand unbroken, though. While surely they will eventually be surpassed by a more advanced aircraft, for now this airplane remains the king of speed in the skies.
Description [ edit | edit source ]
The famous Clarence "Kelly" Johnson is the name behind many of the advanced concepts of aerodynamics that airplane. Its fuselage was made of alloys titanium to withstand the high temperatures around 200-300 degrees Celsius caused by air friction
due to the high speed attained.
As its fuselage was made on plates in order to swell during the flight, the SR-71 is known to leak when they're down, by its hydraulic fluid freeze at temperatures of 30 °C and the peculiar mode of activation of the engines. Because the J-58 turbine large and too heavy (9-stage axial flow compression) to a common pneumatic system, the activation was done by a V-8 engine poisoned by gears connected directly to the turbine shaft in the first years (now the activation was done otherwise written below).
His flight at high temperatures would not be possible without the special fuel developed for him, the JP-7 and little sticky so volatile that it was possible to erase easily a match in a bucket of JP-7. JP-7 not burning with the engine cold, so at the hour of departure was necessary to preheat the turbines with another "formula for witch," the Trimethyl borate - that was a characteristic green flame. For the fuselage, all supersonic aircraft need sharp edges on the cockpit, engines and wings, wich the SR-71 is no exception.
The Blackbird was originally built with a nacelle, for only one pilot, were named A-12 in its second version, called the SR-71, had two nacelles for two crew seats in tandem, leaving the pilot in nacelle front, while the operator of going back in the cockpit. There was also the B version used for training, which had two nacelles, and accommodated two pilots in the cockpit rear was higher for the lead. For missions at high altitudes and speeds, both the crew wore a pressure suit, reminiscent of the early costumes astronauts. For its construction, machines were developed tools (machine tools) with the specific purpose of building components to this plane. When the closure of its production, the machines were destroyed, making it impossible so new parts and / or units of the SR-71 would be made again, and with the end of Cold War, Was no longer viable after using a plane flying hour cost as high.
For various reasons, the SR-71 was disabled. Among them, political factors, operating costs and the advent of satellites. Only three are held in place by NASA to study. This plane was flying so high and so fast that, pursued by a ground to air missile the classic avoidance maneuver was simply to accelerate. Based on Beale in California, The unit equipped with SR-71 were on different bases, mainly in England and Japan, To provide air cover in the world.
SR-71 A-12 YF-12A M-21 The Blackbird Survivors
The SR-71 was a follow-on project to the U-2 aircraft, which evolved from a need for the intelligence agencies to overfly the Soviet Union to determine if the so-called 'bomber gap' was real. The Soviets quickly figured out how to bring down the U-2, so the CIA asked the Lockheed Skunkworks to come up with an aircraft that could overfly hostile territory without risk of being shot down. The airplane that emerged from designer Kelly Johnson's drawing board was a black titanium jet that could fly at Mach 3 at altitudes above 80,000 feet. The theory was very simple. Even if you saw the SR-71 coming, by the time you could launch a missile, the Blackbird would be so far away that the missile would never catch up.
The first group of Blackbirds was built for the CIA under the designation A-12. This single seat version of the Blackbird first flew on April 26, 1962. The Air Force also purchased a group of Blackbirds. They were to be called recon-strike aircraft, but due to a mix-up, the designation ended up being SR-71. The SR-71 is a two seat aircraft. It first flew on December 22, 1964. The USAF tested the Blackbird as a bomber aircraft. Two YF-12A prototypes were developed. Later, the USAF tried to operate the D-21 drone from a Blackbird. The motherships were given the designation M-21. The M-21 program ended in disaster, so the drone role was shifted to B-52 bombers.
The CIA ended its Blackbird operations in 1968. The USAF took over this intelligence gathering role, and continued to operate the Blackbird well into the 1990s. The USAF attempted to retire the Blackbirds due to the extreme cost of the program. The idea was that satellite technology could fill that role. Congress, however, felt otherwise, and continued to fund the SR-71, so the SR-71 was brought back on-line. The aircraft were finally retired a few years later, and several examples were transferred to NASA. The last NASA flight was at the annual Edwards Air Force Base Open House on October 9, 1999. Click here for a photo tour of the final Blackbird flight.
All surviving Blackbirds have now been transferred to museums. Several SR-71s were being held in flyable storage in the event that world events required that they be activated, but those aircraft were released to museums in the mid-2000s. A list of all known Blackbird survivors follows below, along with a hot-link to a page with a photo of each aircraft. So far, I have visited and photographed all but 2 surviving Blackbirds. A few more have moved to new locations since I have last seen them.
This serial number table is based on a list created by Albert Dobyns. It is used with permission. Note that SR-71 serial numbers are often listed as 64-17xxx. These numbers are incorrect, and are often used as disinformation. The correct serial numbers are 61-7xxx.
The SR-71 Spy Plane Was the Jet Russia Never Could Copy
During the Cold War, the United States Air Force had the Lockheed SR-71 spy plane. Unofficially known as the “Blackbird” for its black paint job, which was developed to dissipate heat, it was the fastest plane in the air and even today it remains the fastest production aircraft ever to take to the skies.
Developed in secret by Lockheed “Skunk Works” in the 1950s, the SR-71 could cruise to 80,000 feet above the earth, near the edge of space, and out fly any missile that was launched at it. With no armament, speed was its only defense, but the Blackbird, which first took flight in 1964, was so fast that it could enter hostile airspace, take a series of reconnaissance photos and be well on its way before an adversary could react.
The Soviets countered with the Mikoyan-Gurevich MiG-25, which became one of the fastest military combat aircraft ever produced. Unlike the SR-71 Blackbird, which relied on speed alone, the MiG-25 Foxbat could reach speeds of Mach 3.2 – albeit with the potential risk to the aircraft and its engine – and still carried four R-40 air-to-air missiles equipped with infrared and radar homing heads to shoot down the Blackbird if necessary.
Where the Soviets succeeded with the MiG-25, they actually failed when it came to developing any reconnaissance aircraft nearly as fast as the Blackbird.
This was the Tsybin RSR – “Reactivnyi Strategicheskii Razvedchik” or Russian for “jet strategic reconnaissance” – a Soviet design for an advanced, long-range Mach 3 strategic reconnaissance aircraft. While it is easy to see that it had similarities with the SR-71, it is actually worth noting that that the RSR was developed before Lockheed undertook its efforts to develop the Blackbird.
In fact, the Soviet design bureau took up its task – under the leadership of aviation designer Pavel Tysbin – to develop a ramjet aircraft in 1954 the concept was for a supersonic strategic bomber that could travel at three times the speed of sound. The aircraft as planned would have a maximum range of 10,000 miles and a service ceiling of 98,000 feet. It could have carried intercontinental nuclear strikes at speeds and altitudes nearly impossible to stop.
However, what looks good on the drawing board isn’t always as easy to transform into a functional aircraft. It should be noted that this was just barely a decade after the first jet combat fighters in the RAF’s Gloster Meteor and German Me262 became the world’s first operational jet-powered fighter aircraft. Moreover, it was just barely over fifty years since the Wright Brothers’ first flight!
As the design matured it was determined that the aircraft wouldn’t have quite the range Tysbin envisioned, and couldn’t return to base if used in an intercontinental mission. The design was revised into a reconnaissance aircraft where turbofans could be used for take-off, while the ramjets would be employed once in the air. The RSR would then have a cruising speed above Mach 2 and a service ceiling of 73,800 feet but a range of just 2,500 miles.
The RSR underwent a series of redesigns. But the aircraft barely progressed beyond the prototype stage. In April 1961 Premier Nikita Khrushchev, who was more focused on missiles and the Soviet space efforts, canceled the program. Soon after the SR-71 would achieve everything that the RSR failed to do