Accession Number:

AD0607574

Title:

DETAILED ERROR ANALYSIS FOR SPIN-STABILIZED MISSIONS,

Descriptive Note:

Corporate Author:

TRW SPACE TECHNOLOGY LABS LOS ANGELES CALIF

Personal Author(s):

• Lindberg,H. E.

Report Date:

1959-07-22

Pagination or Media Count:

33.0

Abstract:

The note is intended as a computation guide for finding the total velocity error, in both magnitude and direction, for the spin-stabilized portion of satellite and deep-space probe missions. The time sequence of events and spin-up method used are typical of the Able missions, but it is anticipated that only minor modifications will have to be made in order to make computations for other missions. Author

Descriptors:

• *GUIDED MISSILE COMPONENTS
• *LAUNCH VEHICLES
• ERRORS
• STABILIZATION SYSTEMS
• STABILIZATION SYSTEMS
• ARTIFICIAL SATELLITES
• SPACE PROBES
• SPINNING(MOTION)
• ROCKETS
• THRUST
• STAGING
• ALIGNMENT
• LAUNCHING

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE