M2-F3 (original) (raw)


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M2-F3


Part of M2-F2



M2F2  Lifting Body

M2F2 Lifting Body
M2F2 Lifting Body with F-104 Chase Plane
Credit: NASA


American manned spaceplane. 43 launches, 1966.07.12 to 1971.12.21 . The crashed M2-F2 was rebuilt as the M2-F3 with enlarged vertical stabilizers. Maximum speed achieved was Mach 1.6, top altitude 21,800 m.

Status: Operational 1966. Thrust: 26.40 kN (5,935 lbf). Gross mass: 3,600 kg (7,900 lb). Unfuelled mass: 2,300 kg (5,000 lb). Height: 6.77 m (22.21 ft). Span: 2.93 m (9.61 ft).

The final X-30 National Aerospace Plane configuration seemed to owe much to the M2.

Spacecraft delta v: 1,000 m/s (3,200 ft/sec).



Family: Spaceplane, Suborbital, US Rocketplanes. Country: USA. Engines: XLR11. Propellants: Lox/Alcohol. Agency: Northrop. Bibliography: 152, 158, 22, 4348, 48, 49, 97, 6665.


Photo Gallery



M2-F3 M2-F3Credit: © Mark Wade


M2F1 Lifting Body M2F1 Lifting BodyThe M2-F1 was the first lifting body configuration tested. This glider was made from plywood. It was later succeeded by the M2-F2 metal version.Credit: NASA


Lifting Bodies Lifting BodiesManned Lifting BodiesCredit: NASA


M2F3 Lifting Body M2F3 Lifting BodyM2F3 Lifting Body Launch from B-52Credit: NASA



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