Flight Proofing Test Report for Abort Sensing and Control Unit Drawing No. 27-11111-821,
Abstract
The purpose of the report is to describe the test equipment and procedure required for the flight proofing of components of a 'square canister' containing six rate gyro output detectors, thirteen pressure switch output detectors and associated circuitry needed to supply two 'ready-abort' outputs as well as seventeen telemetry outputs. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 30, 1961
- Accession Number
- AD0851201
Entities
People
- F. J. Denneny
- R. N. Galloway
Organizations
- General Dynamics