Encyclopedia Astronautica
Apollo CM Escape Concept



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Apollo CM Escape SC
Escape capsule using Apollo CM studied by Rockwell for NASA for use with the shuttle in the 1970's-80's.
American manned rescue spacecraft. Study 1976. Escape capsule using Apollo command module studied by Rockwell for NASA for use with the shuttle in the 1970's-80's. Mass per crew: 750 kg.

Crew Size: 6. Habitable Volume: 6.17 m3.

Gross mass: 4,500 kg (9,900 lb).
Height: 4.20 m (13.70 ft).
Span: 3.90 m (12.70 ft).

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Associated Countries
See also
  • Rescue In the early 1960's, in the hey-day of the X-20 Dynasoar, it seemed that the US military would naturally keep building military aerospacecraft that would just keep going higher and faster. It was also supposed that the pilot would have to be given the equivalent of an ejection seat - some means of bailing out of the spacecraft in case of catastrophic failure or enemy attack. More...

Associated Launch Vehicles
  • Shuttle American winged orbital launch vehicle. The manned reusable space system which was designed to slash the cost of space transport and replace all expendable launch vehicles. It did neither, but did keep NASA in the manned space flight business for 30 years. Redesign of the shuttle with reliability in mind after the Challenger disaster reduced maximum payload to low earth orbit from 27,850 kg to 24,400 kg. More...

Associated Manufacturers and Agencies
  • NASA American agency overseeing development of rockets and spacecraft. National Aeronautics and Space Administration, USA, USA. More...
  • North American American manufacturer of rockets, spacecraft, and rocket engines. North American, Palmdale, El Segundo. Downey, CA, USA More...

Associated Propellants
  • Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...

Bibliography
  • Kane, Francis X, "A Thirty Year Perspective on Manned Space Safety and Rescue: Where We've Been; Where We Are; Where We Are Going", IAA, IAA 84-270, 1984.

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