This page no longer updated from 31 October 2001. Latest version can be found at Jupiter C

Redstone engine
Redstone engine -

Credit: NASA. 33,508 bytes. 386 x 305 pixels.

Gross Mass: 28,430 kg. Empty Mass: 3,890 kg. Thrust (vac): 42,439 kgf. Isp: 265 sec. Burn time: 155 sec. Propellants: Lox/Hydyne Isp(sl): 235 sec. Diameter: 1.8 m. Span: 4.2 m. Length: 17.6 m. Country: USA. No Engines: 1. A-7 Status: Hardware. Other designations: Juno 1 (retrospectively). Comments: Redstone missile, stretched, modified with different propellants to serve as first stage of IRBM nose cone/orbital test vehicle.
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Last update 12 March 2001.
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© Mark Wade, 2001 .