NASA M2-F1

Last updated
M2-F1
NASA M2-F1.jpg
RoleLifting-body technology demonstrator
Manufacturer Dryden Flight Research Center
Designer Ames Research Center
First flight16 August 1963
Retired16 August 1966
StatusOn display
Primary user NASA
Number built1
Variants Northrop M2-F2
Northrop M2-F3

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. [1]

Contents

Development

The lifting-body concept originated in the mid-1950s at the National Advisory Committee for Aeronautics' Ames Aeronautical Laboratory, Mountain View, California. By February 1962, a series of possible shapes had been developed, and R. Dale Reed was working to gain support for a research vehicle.

The construction of the M2-F1 was a joint effort by Dryden and a local glider manufacturer, the Briegleb Glider Company. The budget was US$30,000. NASA craftsmen and engineers built the tubular steel interior frame. Its mahogany plywood shell was handmade by Gus Briegleb and company. Ernie Lowder, a NASA craftsman who had worked on Howard Hughes's H-4 Hercules ("Spruce Goose"), was assigned to help Briegleb.

Final assembly of the remaining components (including aluminum tail surfaces, pushrod controls, and landing gear from a Cessna 150, later replaced by Cessna 180 landing gear [2] ) was done at the NASA facility.

The wingless, lifting-body aircraft design was initially conceived as a means of landing a spacecraft horizontally after atmospheric reentry. The absence of wings would make the extreme heat of reentry less damaging to the vehicle. Rather than using a ballistic reentry trajectory like a Command Module, very limited in maneuvering range, a lifting-body vehicle had a landing footprint of the size of California.

Tow testing

The M2-F1 and its 1963 Pontiac convertible tow vehicle M2-F1 with towing car.jpg
The M2-F1 and its 1963 Pontiac convertible tow vehicle

The first flight tests of the M2-F1 were at Rogers Dry Lake, at the end of a tow rope attached to a 1963 Pontiac Catalina convertible. On April 5, 1963 test pilot Milt Thompson lifted the M2-F1's nose off the ground for the first time while being towed. [2] The speed was 86 miles per hour (138 km/h). The little craft seemed to bounce uncontrollably between the main landing gear wheels, and stopped when he lowered the nose to the ground. He tried again, but each time with the same results. He felt it was a landing gear problem that could have caused the aircraft to roll on its back if he had lifted the main gear off the ground.

After looking at movies of the tests, it was decided that the bouncing was probably caused by unwanted rudder movements. The control system was modified so that the joystick controlled the elevons rather than the rudder, which solved the problem.

It was found that the car used to tow the aircraft was not powerful enough to lift the M2-F1 entirely off the ground, so the FRC arranged to have the tow car hot-rodded by Bill Straub: the modifications tuned the engine for increased power, added a rollbar, and turned the front passenger seat to face aft so the passenger could observe the aircraft. This proved successful, and tow tests continued. [2]

Speeds on tow inched up to 110 miles per hour (180 km/h), which allowed Thompson to climb to about 20 feet (6.1 m), then glide for about 20 seconds after releasing the line. That was the most that could be expected during an auto tow.

M2-F1 in tow behind a NASA R4D tow plane. M2-F1 in Tow - GPN-2000-000097.jpg
M2-F1 in tow behind a NASA R4D tow plane.

These initial tests produced enough flight data about the M2-F1 to proceed with flights behind a NASA R4D tow plane at greater altitudes [3] .

Flight testing

A NASA R4D, the Navy designation for the Douglas DC-3, was used for all of the air tows. The first was on August 16, 1963. The M2-F1 had recently been equipped with an ejection seat and small rockets – referred to by the test team as "instant L/D" [2] – in the tail to extend the landing flare for about 5 seconds if needed, and Thompson prepared for the flight with a few more tows behind the Pontiac.

Forward visibility in the M2-F1 was very limited on tow, requiring Thompson to fly about 20 feet (6.1 m) higher than the C-47, so he could see the plane through the nose window. Towing speed was about 100 miles per hour (160 km/h).

The C-47 took the craft to an altitude of 12,000 feet (3,700 m), where free flights back to Rogers Dry Lake began. Pilot for the first series of flights of the M2-F1 was NASA research pilot Milt Thompson. Typical glide flights with the M2-F1 lasted about two minutes and reached speeds of 110 to 120 miles per hour (180 to 190 km/h).

Tow release was at 12,000 feet (3,700 m). The lifting body descended at an average rate of about 3,600 feet per minute (1,100 m/min). At 1,000 feet (300 m) above the ground, the nose was lowered to increase speed to about 150 miles per hour (240 km/h), flare was at 200 feet (61 m) from a 20° dive. The landing was smooth, and the lifting-body program was on its way.

The M2-F1 was flown until August 16, 1966. It proved the lifting-body concept and led the way for subsequent metal "heavyweight" designs. Chuck Yeager, Bruce Peterson and Donald L. Mallick also flew the M2-F1.

More than 400 ground tows and 77 aircraft tow flights were carried out with the M2-F1. The success of Dryden's M2-F1 program led to NASA's development and construction of two heavyweight lifting bodies based on studies at NASA's Ames and Langley research centers – the Northrop M2-F2 and the Northrop HL-10, both built by the Northrop Corporation, and the U.S. Air Force's X-24 program. The lifting-body program also heavily influenced the Space Shuttle program.

The M2-F1 program demonstrated the feasibility of the lifting-body concept for horizontal landings of atmospheric entry vehicles. It also demonstrated a procurement and management concept for prototype flight research vehicles that produced rapid results at very low cost (approximately US$50,000, excluding salaries of government employees assigned to the project).

Pilots

Aircraft serial number

Aircraft on display

As of January 23, 2015, M2-F1 N86652 is on display at the Air Force Flight Test Museum on Edwards Air Force Base, California. [4]

Specifications

NASA M2-F1 lifting-body diagram NASA M2-F1 diagram.png
NASA M2-F1 lifting-body diagram

General characteristics

Performance

Flights

Vehicle
Flight #
DatePilotDurationVelocity
(km/h)
Altitude
(m)
Comments
M2-F1 #0March 1, 1963Thompson-1350First Ground Tow.
400 total ground tows.
M2-F1 #1August 16, 1963Thompson0:02:002403,650First M2-F1 Flight. 77 total flights.
M2-F1 #2August 28, 1963Thompson0:02:092403,650-
M2-F1 #3August 29, 1963Thompson0:02:252403,650-
M2-F1 #4August 30, 1963Thompson0:04:422403,6501st flight of day
M2-F1 #5August 30, 1963Thompson-2403,6502nd flight of day
M2-F1 #6September 3, 1963Thompson0:04:502403,6501st flight of day
M2-F1 #7September 3, 1963Thompson-2403,6502nd flight of day
M2-F1 #8October 7, 1963Thompson0:01:262403,650-
M2-F1 #9October 9, 1963Thompson0:01:512403,650-
M2-F1 #10October 15, 1963Thompson0:02:202403,650-
M2-F1 #11October 23, 1963Thompson0:03:002403,650-
M2-F1 #12October 25, 1963Thompson0:03:522403,6501st flight of the day
M2-F1 #13October 25, 1963Thompson-2403,6502nd flight of the day
M2-F1 #14November 8, 1963Thompson0:07:452403,6501st flight of the day
M2-F1 #15November 8, 1963Thompson-2403,6502nd flight of the day
M2-F1 #16November 8, 1963Thompson-2403,6503rd flight of the day
M2-F1 #17December 3, 1963Thompson0:01:002403,650-
M2-F1 #18December 3, 1963Yeager0:01:352403,650-
M2-F1 #19December 3, 1963Peterson0:03:152403,6501st flight of the day
M2-F1 #20December 3, 1963Peterson-2403,6502nd flight of the day
Broke landing gear
M2-F1 #21January 29, 1964Thompson-2403,6501st flight of the day
M2-F1 #22January 29, 1964Thompson-2403,6502nd flight of the day
M2-F1 #23January 29, 1964Peterson0:04:442403,6501st flight of the day
M2-F1 #24January 29, 1964Peterson-2403,6502nd flight of the day
M2-F1 #25January 29, 1964Yeager-2403,6501st flight of the day
M2-F1 #26January 29, 1964Yeager-2403,6502nd flight of the day
M2-F1 #27January 30, 1964Yeager-2403,6501st flight of the day
M2-F1 #28January 30, 1964Yeager-2403,6502nd flight of the day
M2-F1 #29January 30, 1964Mallick-2403,6501st flight of the day
M2-F1 #30January 30, 1964Mallick-2403,6502nd flight of the day
M2-F1 #31February 28, 1964Thompson-2403,6501st flight of the day
M2-F1 #32February 28, 1964Thompson-2403,6502nd flight of the day
M2-F1 #33March 30, 1964Peterson0:02:252403,650-
M2-F1 #34April 9, 1964Thompson-2403,6501st flight of the day
M2-F1 #35April 9, 1964Thompson-2403,6502nd flight of the day
M2-F1 #36April 9, 1964Peterson0:08:002403,6501st flight of the day
M2-F1 #37April 9, 1964Peterson-2403,6502nd flight of the day
M2-F1 #38April 9, 1964Peterson-2403,6503rd flight of the day
M2-F1 #39May 19, 1964Peterson0:04:082403,6501st flight of the day
M2-F1 #40May 19, 1964Peterson-2403,6502nd flight of the day
M2-F1 #41June 3, 1964Thompson-2403,650-
M2-F1 #42July 24, 1964Peterson0:06:502403,6501st flight of the day
M2-F1 #43July 24, 1964Peterson-2403,6502nd flight of the day
M2-F1 #44July 24, 1964Peterson-2403,6503rd flight of the day
M2-F1 #45August 18, 1964Thompson-2403,650-
M2-F1 #46August 21, 1964Thompson-2403,6501st flight of the day
M2-F1 #47August 21, 1964Thompson-2403,6502nd flight of the day
M2-F1 #48August 21, 1964Thompson-2403,6503rd flight of the day
M2-F1 #49August 21, 1964Thompson-2403,6504th flight of the day
M2-F1 #50February 16, 1965Thompson-2403,650-
M2-F1 #51May 27, 1965Thompson-2403,6501st flight of the day
M2-F1 #52May 27, 1965Thompson-2403,6502nd flight of the day
M2-F1 #53May 27, 1965Thompson-2403,6503rd flight of the day
M2-F1 #54May 27, 1965Thompson-2403,6504th flight of the day
M2-F1 #55May 27, 1965Sorlie0:06:002403,6501st flight of the day
M2-F1 #56May 27, 1965Sorlie-2403,6502nd flight of the day
M2-F1 #57May 27, 1965Sorlie-2403,6503rd flight of the day
M2-F1 #58May 28, 1965Thompson-2403,650-
M2-F1 #59May 28, 1965Sorlie0:04:302403,6501st flight of the day
M2-F1 #60May 28, 1965Sorlie-2403,6502nd flight of the day
M2-F1 #61July 16, 1965Thompson-2403,650-
M2-F1 #62July 16, 1965Dana-2403,650-
M2-F1 #63July 16, 1965Gentry0:00:0920010Rolled M2-F1 on liftoff.
Recovered. Safe landing.
M2-F1 #64August 30, 1965Thompson-2403,6501st flight of the day
M2-F1 #65August 30, 1965Thompson-2403,6502nd flight of the day
M2-F1 #66August 30, 1965Thompson-2403,6503rd flight of the day
M2-F1 #67August 31, 1965Thompson-2403,650-
M2-F1 #68October 6, 1965Thompson-2403,6501st flight of the day
M2-F1 #69October 6, 1965Thompson-2403,6502nd flight of the day
M2-F1 #70October 8, 1965Thompson-2403,650-
M2-F1 #71March 28, 1966Thompson-2403,6501st flight of the day
M2-F1 #72March 28, 1966Thompson-2403,6502nd flight of the day
M2-F1 #73August 4, 1966Peterson0:02:002403,650-
M2-F1 #74August 5, 1966Peterson0:04:002403,6501st flight of the day
M2-F1 #75August 5, 1966Peterson-2403,6502nd flight of the day
M2-F1 #76August 5, 1966Peterson-2403,6503rd flight of the day
M2-F1 #77August 16, 1966Gentry-20010Rolled M2-F1 on liftoff. Recovered.
Fired landing rockets.
Safe landing. Last flight.

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

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">Armstrong Flight Research Center</span> United States aerospace research facility

The NASA Neil A. Armstrong Flight Research Center (AFRC) is an aeronautical research center operated by NASA. Its primary campus is located inside Edwards Air Force Base in California and is considered NASA's premier site for aeronautical research. AFRC operates some of the most advanced aircraft in the world and is known for many aviation firsts, including supporting the first crewed airplane to exceed the speed of sound in level flight, highest speed by a crewed, powered aircraft, the first pure digital fly-by-wire aircraft, and many others. AFRC operates a second site next to Air Force Plant 42 in Palmdale, California, known as Building 703, once the former Rockwell International/North American Aviation production facility. There, AFRC houses and operates several of NASA's Science Mission Directorate aircraft including SOFIA, a DC-8 Flying Laboratory, a Gulfstream C-20A UAVSAR and ER-2 High Altitude Platform. As of 2023, Bradley Flick is the center's director.

<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">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

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> Type of aircraft

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">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">Northrop M2-F3</span> Lifting body prototype aircraft

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.

<span class="mw-page-title-main">Shuttle Training Aircraft</span> Training aircraft for the Space Shuttle

The Shuttle Training Aircraft (STA) is a former NASA training vehicle that duplicated the Space Shuttle's approach profile and handling qualities, allowing pilots to simulate Shuttle landings under controlled conditions before attempting the task on board the orbiter. The STA was also flown to assess weather conditions just prior to Space Shuttle launches and landings.

<span class="mw-page-title-main">NASA Paresev</span> Experimental NASA glider using the Rogallo airfoil

The NASA Paresev was an experimental NASA glider aircraft based upon the kite-parachute studies by NASA engineer Francis Rogallo.

<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.

The Rans S-11 Pursuit is an American single-engined, tractor configuration, single-seat, low-wing aircraft, based on the lifting body principle, designed and built by Randy Schlitter. The Pursuit was listed as under development in 1998, but only prototypes were ever completed and the aircraft is not part of the present Rans aircraft line.

<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">Drop test</span> Method of testing aircraft/spacecraft

A drop test is a method of testing the in-flight characteristics of prototype or experimental aircraft and spacecraft by raising the test vehicle to a specific altitude and then releasing it. Test flights involving powered aircraft, particularly rocket-powered aircraft, may be referred to as drop launches due to the launch of the aircraft's rockets after release from its carrier aircraft.

References

  1. Reed, R. Dale; Darlene Lister (2002). Wingless Flight: The Lifting Body Story. University Press of Kentucky. ISBN   0-8131-9026-6.
  2. 1 2 3 4 Jenkins, Dennis R. (2001). Space Shuttle: The History of the National Space Transportation System (3rd ed.). Voyageur Press. ISBN   0-9633974-5-1.
  3. "Where Are They Now: M2-F1 Lifting Body - NASA" . Retrieved 2024-02-08.
  4. Project Habu: M2-F1