Accession Number:

AD0851391

Title:

Control-Rate of Turn, Autopilot CVA Part No. 27-04574-1.

Descriptive Note:

Evaluation test rept.,

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-03-27

Pagination or Media Count:

58.0

Abstract:

The purpose of the report is to describe the test equipment, test procedure, and results of the evaluation testing of an angular rate gyro.

Subject Categories:

  • Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE