TEST REPORT, INSTRUMENTATION FLIGHT PROOF TEST (CTL) - (10-20885-1 C/D RECEIVER CONFIG.),
Abstract
This document contains the test report of the Flight Proof Test of the MRCN 6301 Minuteman WS-133A CTLI configuration using the 10-20885 specification Command-Destruct receivers. This configuration is representative of a number of flight wafer, MRCN 6301, numbered above 0000017. Only equipment which was not qualified in pre vious Flight Proof Testing was installed and oper ated during this test. All other equipment was size and mass simulated. The Flight Proof Test consisted of the following tests: Drop Test (Un packaged), Vibration Test (Non-Operation), Flight Vibration Test (Operating). The Flight Proof Test Program is intended to assure and demon strate system design capability of the Boeing assembled CTLI System preparatory to flight tests. The program is intended to demonstrate both reli ability and accuracy of performance of the CTLI System under laboratory produced environmental conditions simulating environments expected dur ing shipping to the test site, and during han dling, storage, testing and flight. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 09, 1963
- Accession Number
- AD0413322
Entities
People
- J. Farrell
Organizations
- Boeing