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Hywards
Part of Dynasoar
American manned combat spacecraft. Study 1956. Hypersonic manned test spaceplane project of the 1950's. Predecessor to Dynasoar.

AKA: Hypersonic Weapon And R&D System. Status: Study 1956.

On 6 November 1956 the USAF issued SR-131 for the 455L HYWARDS Hypersonic Weapon And R&D System - an experimental spaceplane to support development of an operational Robo/Brass Bell bomber. HYWARDS was to be capable of carrying out flight research up to Mach 15 and also provide a vehicle to test operational subsystems. Engines considered for the booster included the Chariot 15,900 kgf LF2/Ammonia engine from Bell; the 25,000 kgf LR-105 Atlas sustainer engine; the 27,000 kgf LR-91 Titan I second stage engine; or the 26,000 kgf XLR-99 X-15 engine. Maximum velocity was to be 3.7 km/s at 110 km altitude. First flights would be air-launched. Later tests would be boosted by an ICBM from a launch pad at Cape Canaveral. On 17 June 1957 NACA Langley completed configuration analysis for the spaceplane. For the planned Mach 18 maximum heating velocity at 5000 km range, they recommended a flat-bottomed, delta-shaped vehicle, with the fuselage on the lee side. The hot structure would be water-cooled. By contrast the alternate NACA Ames vehicle design was planned for a maximum of Mach 10 and 3200 km range. It used a mid-wing design, which would result in extreme heating on the fuselage. Langley felt that the cooling requirements of this configuration outweighed the L/D advantage of the aerodynamic configuration. HYWARDS was rolled into the Dynasoar program in October 1957.



Family: Combat spacecraft, US Rocketplanes. Country: USA. Agency: NASA. Bibliography: 44.

1956 March 1 - .
1956 November 6 - .
1957 April 30 - .
1957 October 10 - .

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