SUSTAINER ENGINE CONTROL SYSTEM SHUTDOWN CHARACTERISTICS WITH HYDRAULIC FAILURE, WS107A,
Abstract
This test procedure corroborates the integrity of a liquid rocket sustainer engine hydraulic accumulator relative to control systems pressure decay.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 12, 1959
- Accession Number
- AD0833245
Entities
People
- P. S. Shannon
Organizations
- General Dynamics