M2-F3 | |
---|---|
General information | |
Type | Lifting body technology demonstrator |
Manufacturer | Northrop |
Status | Donated to the Smithsonian Institution, currently on display at the National Air and Space Museum |
Primary user | NASA |
History | |
First flight | 2 June 1970 |
Retired | 20 December 1972 |
Developed from | NASA M2-F1 Northrop M2-F2 |
The Northrop M2-F3 was a heavyweight lifting body rebuilt from the Northrop M2-F2 after it crashed at the Dryden Flight Research Center in 1967. It was modified with an additional third vertical fin - centered between the tip fins - to improve control characteristics. The "M" refers to "manned" and "F" refers to "flight" version.
Early flight testing of the M2-F1 and M2-F2 lifting body reentry configurations had validated the concept of piloted lifting body reentry from space. When the M2-F2 crashed on May 10, 1967, valuable information had already been obtained and was contributing to new designs.
NASA pilots said the M2-F2 had lateral control problems, so when the M2-F2 was rebuilt at Northrop and redesignated the M2-F3, it was modified with an additional third vertical fin - centered between the tip fins - to improve control characteristics.
After a three-year-long redesign and rebuilding effort, the M2-F3 was ready to fly. The May 1967 crash of the M2-F2 had torn off the left fin and landing gear. It had also damaged the external skin and internal structure. Flight Research Center engineers worked with Ames Research Center and the Air Force in redesigning the vehicle with a center fin to provide greater stability. At first, it seemed that the vehicle had been irreparably damaged, but the original manufacturer, Northrop, did the repair work and returned the redesigned M2-F3 with a center fin for stability to the FRC.
While the M2-F3 was still demanding to fly, the center fin eliminated the high risk of pilot-induced oscillation (PIO) that was characteristic of the M2-F2.
First flight of the M2-F3, with NASA pilot Bill Dana at the controls, was June 2, 1970. The modified vehicle exhibited much better lateral stability and control characteristics than before, and only three glide flights were necessary before the first powered flight on November 25, 1970. The 100th flight of the heavy-weight lifting bodies was completed on October 5, 1972, with pilot Bill Dana soaring to an altitude of 66,300 feet (20,200 m) and a Mach number of 1.370 (about 904 miles per hour (1,455 km/h)) in the M2-F3. Over its 27 missions, the M2-F3 reached a top speed of 1,064 mph (1,712 km/h) (Mach 1.6). Highest altitude reached by the vehicle was 71,500 feet (20,790 m) on December 20, 1972, the date of its last flight, with NASA pilot John Manke at the controls.
A reaction control thruster (RCT) system, similar to that on orbiting spacecraft, was also installed to obtain research data about their effectiveness for vehicle control. As the M2-F3's portion of the lifting body program neared an end, it evaluated a rate command augmentation control system, and a side control stick similar to side-stick controllers now used on many modern aircraft.
NASA donated the M2-F3 vehicle to the Smithsonian Institution in December 1973. It is currently hanging in the National Air and Space Museum along with the X-15 aircraft number 1, which was its hangar partner at Dryden from 1965 to 1969.
Vehicle Flight # | Date | Pilot | Mach | Velocity (km/h) | Altitude | Duration | Comments | |
---|---|---|---|---|---|---|---|---|
ft | m | |||||||
M2-F3 #1 | June 2, 1970 | Dana | 0.688 | 755 | 45,000 | 14,000 | 00:03:38 | First M2-F3 Flight Unpowered glide |
M2-F3 #2 | July 21, 1970 | Dana | 0.660 | 708 | 45,000 | 14,000 | 00:03:48 | Unpowered glide |
M2-F3 #3 | November 2, 1970 | Dana | 0.630 | 690 | 45,000 | 14,000 | 00:03:56 | Unpowered glide |
M2-F3 #4 | November 25, 1970 | Dana | 0.809 | 859 | 51,900 | 15,800 | 00:06:17 | 1st powered flight |
M2-F3 #5 | February 9, 1971 | Gentry | 0.707 | 755 | 45,000 | 14,000 | 00:04:01 | - |
M2-F3 #6 | February 26, 1971 | Dana | 0.773 | 821 | 45,000 | 14,000 | 00:05:48 | Only 2 chambers lit |
M2-F3 #7 | July 23, 1971 | Dana | 0.930 | 988 | 60,500 | 18,400 | 00:05:53 | - |
M2-F3 #8 | August 9, 1971 | Dana | 0.974 | 1,035 | 62,000 | 19,000 | 00:06:55 | - |
M2-F3 #9 | August 25, 1971 | Dana | 1.095 | 1,164 | 67,300 | 20,500 | 00:06:30 | 1st supersonic flight |
M2-F3 #10 | September 24, 1971 | Dana | 0.728 | 772 | 42,000 | 13,000 | 00:03:30 | Engine fire |
M2-F3 #11 | November 15, 1971 | Dana | 0.739 | 784 | 45,000 | 14,000 | 00:03:35 | - |
M2-F3 #12 | December 1, 1971 | Dana | 1.274 | 1,357 | 70,800 | 21,600 | 00:06:31 | - |
M2-F3 #13 | December 16, 1971 | Dana | 0.811 | 861 | 46,800 | 14,300 | 00:07:31 | Only 2 chambers lit |
M2-F3 #14 | July 25, 1972 | Dana | 0.989 | 1,049 | 60,900 | 18,600 | 00:07:00 | - |
M2-F3 #15 | August 11, 1972 | Gentry | 1.101 | 1,168 | 67,200 | 20,500 | 00:06:15 | - |
M2-F3 #16 | August 24, 1972 | Dana | 1.266 | 1,344 | 66,700 | 20,300 | 00:06:16 | - |
M2-F3 #17 | September 12, 1972 | Dana | 0.880 | 935 | 46,000 | 14,000 | 00:06:27 | Small engine fire |
M2-F3 #18 | September 27, 1972 | Dana | 1.340 | 1,424 | 66,700 | 20,300 | 00:06:07 | - |
M2-F3 #19 | October 5, 1972 | Dana | 1.370 | 1,455 | 66,300 | 20,200 | 00:06:16 | 100th lifting body flight |
M2-F3 #20 | October 19, 1972 | Manke | 0.905 | 961 | 47,100 | 14,400 | 00:05:59 | - |
M2-F3 #21 | November 1, 1972 | Manke | 1.213 | 1,292 | 71,300 | 21,700 | 00:06:18 | - |
M2-F3 #22 | November 9, 1972 | Powell | 0.906 | 961 | 46,800 | 14,300 | 00:06:04 | - |
M2-F3 #23 | November 21, 1972 | Manke | 1.435 | 1,524 | 66,700 | 20,300 | 00:06:17 | Planned Rosamond Lakebed landing |
M2-F3 #24 | November 29, 1972 | Powell | 1.348 | 1,432 | 67,500 | 20,600 | 00:05:57 | - |
M2-F3 #25 | December 6, 1972 | Powell | 1.191 | 1,265 | 68,300 | 20,800 | 00:05:32 | Planned Rosamond Lakebed landing |
M2-F3 #26 | December 13, 1972 | Dana | 1.613 | 1,712 | 66,700 | 20,300 | 00:06:23 | Fastest flight |
M2-F3 #27 | December 20, 1972 | Manke | 1.294 | 1,378 | 71,500 | 21,800 | 00:06:30 | Highest flight Last M2-F3 flight |
Data from[ citation needed ]
General characteristics
Performance
Comparable aircraft:
A lifting body is a fixed-wing aircraft or spacecraft configuration in which the body itself produces lift. In contrast to a flying wing, which is a wing with minimal or no conventional fuselage, a lifting body can be thought of as a fuselage with little or no conventional wing. Whereas a flying wing seeks to maximize cruise efficiency at subsonic speeds by eliminating non-lifting surfaces, lifting bodies generally minimize the drag and structure of a wing for subsonic, supersonic and hypersonic flight, or spacecraft re-entry. All of these flight regimes pose challenges for proper flight safety.
The Martin Marietta X-24 was an American experimental aircraft developed from a joint United States Air Force-NASA program named PILOT (1963–1975). It was designed and built to test lifting body concepts, experimenting with the concept of unpowered reentry and landing, later used by the Space Shuttle. Originally built as the X-24A, the aircraft was later rebuilt as the X-24B.
The Northrop YF-17 was a prototype lightweight fighter aircraft designed by Northrop aviation for the United States Air Force's Lightweight Fighter (LWF) technology evaluation program. The LWF was initiated because many in the fighter community believed that aircraft like the F-15 Eagle were too large and expensive for many combat roles. The YF-17 was the culmination of a long line of Northrop designs, beginning with the N-102 Fang in 1956, continuing through the F-5 family.
The Northrop X-4 Bantam was a prototype small twinjet aircraft manufactured by Northrop Corporation in 1948. It had no horizontal tail surfaces, depending instead on combined elevator and aileron control surfaces for control in pitch and roll attitudes, almost exactly in the manner of the similar-format, rocket-powered Messerschmitt Me 163 of Nazi Germany's Luftwaffe. Some aerodynamicists had proposed that eliminating the horizontal tail would also do away with stability problems at fast speeds resulting from the interaction of supersonic shock waves from the wings and the horizontal stabilizers. The idea had merit, but the flight control systems of that time prevented the X-4 from achieving any success.
The Grumman X-29 was an American experimental aircraft that tested a forward-swept wing, canard control surfaces, and other novel aircraft technologies. Funded by NASA, the United States Air Force and DARPA, the X-29 was developed by Grumman, and the two built were flown by NASA and the United States Air Force. The aerodynamic instability of the X-29's airframe required the use of computerized fly-by-wire control. Composite materials were used to control the aeroelastic divergent twisting experienced by forward-swept wings, and to reduce weight. The aircraft first flew in 1984, and two X-29s were flight tested through 1991.
The McDonnell DouglasX-36Tailless Fighter Agility Research Aircraft was an American stealthy subscale prototype jet designed to fly without the traditional empennage found on most aircraft. This configuration was designed to reduce weight, drag and radar cross section, and increase range, maneuverability and survivability.
The Rockwell-Messerschmitt-Bölkow-Blohm X-31 is an experimental jet aircraft designed to test fighter thrust vectoring technology. It was designed and built by Rockwell and Messerschmitt-Bölkow-Blohm (MBB), as part of a joint US and German Enhanced Fighter Maneuverability program to provide additional control authority in pitch and yaw, for significantly more maneuverability than most conventional fighters. An advanced flight control system provided controlled flight at high angles of attack where conventional aircraft would stall or lose control. Two aircraft were built, of which only one has survived.
The Boeing X-48 is an American experimental unmanned aerial vehicle (UAV) built to investigate the characteristics of blended wing body (BWB) aircraft. Boeing designed the X-48 and two examples were built by Cranfield Aerospace in the UK. Boeing began flight testing the X-48B version for NASA in 2007. The X-48B was later modified into the X-48C version, which was flight tested from August 2012 to April 2013. Boeing and NASA plan to develop a larger BWB demonstrator.
The X-38 was an experimental re-entry vehicle designed by NASA to research a possible emergency crew return vehicle (CRV) for the International Space Station (ISS). The 1995–2002 program also developed concepts for a crew return vehicle design that could be modified for other uses, such as a possible joint U.S. and international human spacecraft that could be launched on the French Ariane 5 booster.
William Harvey Dana was an American aeronautical engineer, U.S. Air Force pilot, NASA test pilot, and astronaut. He was one of twelve pilots who flew the North American X-15, an experimental spaceplane jointly operated by the Air Force and NASA. He was also selected for participation in the X-20 Dyna-Soar program.
Milton Orville Thompson, , better known as Milt Thompson, was an American naval officer, aviator, engineer, and NASA research pilot. He was one of twelve pilots who flew the North American X-15, an experimental spaceplane jointly operated by the United States Air Force and NASA.
The Scaled Composites Model 281 Proteus is a tandem-wing high-altitude long-endurance aircraft designed by Burt Rutan to investigate the use of aircraft as high-altitude telecommunications relays. The Proteus is a multi-mission vehicle able to carry various payloads on a ventral pylon. The Proteus has an extremely efficient design and can orbit a point at over 19,800 m for more than 18 hours. It is currently owned by Northrop Grumman.
Bruce A. Peterson was an American aeronautical engineer, and test pilot for NASA.
The Northrop HL-10 was one of five US heavyweight lifting body designs flown at NASA's Flight Research Center in Edwards, California, from July 1966 to November 1975 to study and validate the concept of safely maneuvering and landing a low lift-over-drag vehicle designed for reentry from space. It was a NASA design and was built to evaluate "inverted airfoil" lifting body and delta planform. It currently is on display at the entrance to the Armstrong Flight Research Center at Edwards Air Force Base.
The NASA M2-F1 was a lightweight, unpowered prototype aircraft, developed to flight-test the wingless lifting body concept. Its unusual appearance earned it the nickname "flying bathtub" and was designated the M2-F1, the M referring to "manned", and F referring to "flight" version. In 1962, NASA Dryden management approved a program to build a lightweight, unpowered lifting-body prototype. It featured a plywood shell placed over a tubular steel frame crafted at Dryden. Construction was completed in 1963.
The Northrop M2-F2 was a heavyweight lifting body based on studies at NASA's Ames and Langley research centers and built by the Northrop Corporation in 1966.
The NASA AD-1 was both an aircraft and an associated flight test program conducted between 1979 and 1982 at the NASA Dryden Flight Research Center, Edwards California, which successfully demonstrated an aircraft wing that could be pivoted obliquely from zero to 60 degrees during flight.
Jerauld Richard "Jerry" Gentry was a United States Air Force (USAF) test pilot and Vietnam combat veteran. As chief USAF pilot of the Lifting Body Research Program, he helped validate the concept of flying a wingless vehicle back to Earth from space and landing it like an aircraft—an approach used by the Space Shuttle and to a greater degree by vehicles such as the Lockheed Martin X-33 and NASA X-38. Gentry completed thirty lifting body flights including the first flight of the Martin-Marietta X-24A and the second flight of the Northrop HL-10.
The NASA Hyper III was an American unpowered full-scale lifting body remotely piloted vehicle designed and built at the NASA Flight Research Center at Edwards Air Force Base, California.
SSC Demo-1, also known as Dream Chaser Demo-1, is the planned first flight of the Sierra Space robotic resupply spacecraft Dream Chaser to the International Space Station (ISS) under the CRS-2 contract with NASA. The demonstration mission is planned for launch no earlier than 2025.