IOC-2 LAUNCHER STABILIZING SYSTEM CONFIDENCE TEST PROCEDURE, WS 107A.
Abstract
Design changes necessitate the functional confidence testing of the IOC-2 Launcher Sub Systems under operational loading conditions. This report outlines the test procedure to be followed in testing the stabilizing subsystems. Testing shall be conducted under simulated operational and environmental temperature conditions to insure proper operation and prove component - system compatibility. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 15, 1959
- Accession Number
- AD0832477
Entities
Organizations
- General Dynamics