Accession Number:

ADA123735

Title:

Design and Fabricate Rocket Attitude Control System (ACS) for Accurate Payload Orientation and Control Functions.

Descriptive Note:

Final rept. 10 Aug 77-30 Apr 82,

Corporate Author:

SPACE VECTOR CORP NORTHRIDGE CA

Personal Author(s):

Report Date:

1982-05-14

Pagination or Media Count:

7.0

Abstract:

Three 3 Attitude Control Systems ACS were designed and built for SPICE, IRBS, ZIP, and FIRSSE Background Measurements programs. They utilized star tracker, IRU, and MIDAS platforms. The IRU system gives state-of-the-art accuracy. Author

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE