Northrop M2-F3

Last updated
M2-F3
Northrop M2-F3.jpg
General information
TypeLifting body technology demonstrator
Manufacturer Northrop
StatusDonated to the Smithsonian Institution, currently on display at the National Air and Space Museum
Primary user NASA
History
First flight2 June 1970
Retired20 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.

Contents

Development

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.

Operational history

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.

The M2-F3 at the National Air and Space Museum M2-F2.jpg
The M2-F3 at the National Air and Space Museum

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.

Aircraft serial number

M2-F3 flights

Vehicle
Flight #
DatePilotMachVelocity
(km/h)
AltitudeDurationComments
ftm
M2-F3 #1June 2, 1970Dana0.68875545,00014,00000:03:38First M2-F3 Flight
Unpowered glide
M2-F3 #2July 21, 1970Dana0.66070845,00014,00000:03:48Unpowered glide
M2-F3 #3November 2, 1970Dana0.63069045,00014,00000:03:56Unpowered glide
M2-F3 #4November 25, 1970Dana0.80985951,90015,80000:06:171st powered flight
M2-F3 #5February 9, 1971Gentry0.70775545,00014,00000:04:01-
M2-F3 #6February 26, 1971Dana0.77382145,00014,00000:05:48Only 2 chambers lit
M2-F3 #7July 23, 1971Dana0.93098860,50018,40000:05:53-
M2-F3 #8August 9, 1971Dana0.9741,03562,00019,00000:06:55-
M2-F3 #9August 25, 1971Dana1.0951,16467,30020,50000:06:301st supersonic flight
M2-F3 #10September 24, 1971Dana0.72877242,00013,00000:03:30Engine fire
M2-F3 #11November 15, 1971Dana0.73978445,00014,00000:03:35-
M2-F3 #12December 1, 1971Dana1.2741,35770,80021,60000:06:31-
M2-F3 #13December 16, 1971Dana0.81186146,80014,30000:07:31Only 2 chambers lit
M2-F3 #14July 25, 1972Dana0.9891,04960,90018,60000:07:00-
M2-F3 #15August 11, 1972Gentry1.1011,16867,20020,50000:06:15-
M2-F3 #16August 24, 1972Dana1.2661,34466,70020,30000:06:16-
M2-F3 #17September 12, 1972Dana0.88093546,00014,00000:06:27Small engine fire
M2-F3 #18September 27, 1972Dana1.3401,42466,70020,30000:06:07-
M2-F3 #19October 5, 1972Dana1.3701,45566,30020,20000:06:16100th lifting
body flight
M2-F3 #20October 19, 1972Manke0.90596147,10014,40000:05:59-
M2-F3 #21November 1, 1972Manke1.2131,29271,30021,70000:06:18-
M2-F3 #22November 9, 1972Powell0.90696146,80014,30000:06:04-
M2-F3 #23November 21, 1972Manke1.4351,52466,70020,30000:06:17Planned Rosamond
Lakebed landing
M2-F3 #24November 29, 1972Powell1.3481,43267,50020,60000:05:57-
M2-F3 #25December 6, 1972Powell1.1911,26568,30020,80000:05:32Planned Rosamond
Lakebed landing
M2-F3 #26December 13, 1972Dana1.6131,71266,70020,30000:06:23Fastest flight
M2-F3 #27December 20, 1972Manke1.2941,37871,50021,80000:06:30Highest flight
Last M2-F3 flight

Specifications (M2-F3)

NASA M2-F3 Lifting Body Diagram NASA M2-F3 diagram.png
NASA M2-F3 Lifting Body Diagram

Data from[ citation needed ]

General characteristics

Performance

See also

Comparable aircraft:

Related Research Articles

<span class="mw-page-title-main">Lifting body</span> Aircraft configuration in which the fuselage produces significant lift

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.

<span class="mw-page-title-main">Martin Marietta X-24</span> American experimental aircraft

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.

<span class="mw-page-title-main">Northrop YF-17</span> Prototype fighter aircraft for the US military

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.

<span class="mw-page-title-main">Northrop X-4 Bantam</span> American experimental jet aircraft

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.

<span class="mw-page-title-main">Grumman X-29</span> 1984 experimental aircraft family by Grumman

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.

<span class="mw-page-title-main">McDonnell Douglas X-36</span>

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.

<span class="mw-page-title-main">Rockwell-MBB X-31</span>

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.

<span class="mw-page-title-main">Boeing X-48</span> Airplane

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.

<span class="mw-page-title-main">NASA X-38</span> Experimental space lifeboat vehicle

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.

<span class="mw-page-title-main">William H. Dana</span> NASA research pilot and astronaut (1930–2014)

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.

<span class="mw-page-title-main">Milton Orville Thompson</span> American aviator (1926–1993)

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.

<span class="mw-page-title-main">Scaled Composites Proteus</span> Experimental aircraft

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.

<span class="mw-page-title-main">Bruce Peterson</span>

Bruce A. Peterson was an American aeronautical engineer, and test pilot for NASA.

<span class="mw-page-title-main">Northrop HL-10</span>

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.

<span class="mw-page-title-main">NASA M2-F1</span> Lifting body prototype

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.

<span class="mw-page-title-main">Northrop M2-F2</span> Lifting body prototype

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.

<span class="mw-page-title-main">NASA AD-1</span> NASA experimental oblique wing aircraft

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.

<span class="mw-page-title-main">Jerauld R. Gentry</span> United States Air Force pilot (1935–2003)

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.

<span class="mw-page-title-main">NASA Hyper III</span> Type of aircraft

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.

<span class="mw-page-title-main">SSC Demo-1</span> Planned 2025 American test spaceflight to the ISS

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.