Centaur Propellant Utilization Ratio Error Detector Assembly. Vibration Test Procedure.
Abstract
The purpose was to specify requirements and procedures for testing and checkout of the Centaur ratio error detector assembly during vibration. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 28, 1962
- Accession Number
- AD0843171
Entities
People
- B. A. Lanterman
Organizations
- General Dynamics