Accession Number:

ADA009140

Title:

Solid Motor/Spacecraft Interfaces.

Descriptive Note:

Final rept.,

Corporate Author:

AEROSPACE CORP EL SEGUNDO CALIF ENGINEERING SCIENCE OPERATIONS

Personal Author(s):

Report Date:

1974-11-03

Pagination or Media Count:

13.0

Abstract:

The origin of the requirements and the resulting specifications for solid propellant rocket motors used with spacecraft are discussed. Typical specification values that have been used previously are presented. Specifications discussed are total impulse, thrust level, thrust alignment, temperature, plumes and contamination, spin rate, vibration and shock, center of gravity and balance.

Subject Categories:

  • Solid Propellant Rocket Engines
  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE