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Cover, Rocket Motor Nozzle

Display Status:
This object is not on display at the National Air and Space Museum, it is either on loan or in storage.

Cover, Rocket Motor Nozzle

 

  • Summary

Manufacturer:   The Marquardt Corporation

Country of Origin: United States of America

Dimensions:
Overall (each half x 8): 6 1/2in. x 3 3/8in. x 9 5/8in. (16.51 x 8.57 x 24.45cm)
Storage: 8 1/4in. x 8 1/4in. x 1ft 10in. (20.96 x 20.96 x 55.88cm)

Materials:
Plastic Aluminum Paper Adhesive Ink

This is a quad, or cluster, of four Apollo Reaction Control System (RCS) engines. The RCS was a vital rocket engine system for maintaining the attitude of the Apollo Service Module (SM), helped it to maneuver in space, plus undertake minor midcourse velocity corrections, abort separations and emergency attitude maneuvers. Each thruster produced 100 pounds of thrust. The propellants were monomethyl hydrazine (MMH) and nitrogen tetroxide. The quad shown here was not flown but was from Apollo-Soyuz Test Project, possibly as a backup RCS. It was transferred to the Smithsonian in 1980 from the NASA Johnson Space Flight Center.


Inventory number: A19800081002