MODEL SPECIFICATION - R+D PROTOTYPES FOR WING II MISSILES, S-133-1000-0-1
Abstract
Test requirements for verification of prototype XSM-80B missile design under the flight testing provisions of the WS-133A Research and Develop ment Program were established. Airborne System Requirements - Model Specifiation S-133-1000 0-1 (D2-14286) covers only the production end item, Guided Missile Main Assemblage, delivered less G+C Section and R/V from Air Force Plant 77. This specification (S-133-1000-0-1, D2-14286-1)correlates the planned variations in Wing II R+D flight missile configuration by identification of the Associate Contractor model specifications for major sections of the missile and its operating subsystems. Operating Conditions - Test Direc tives issued in accordance with the WS-133A Gen eral Test Plan will establish the requirements for ground tests utilizingthe XSM-80B missile, and for missile performance and range capability demonstrations to be fired from underground launchers at existing test sites near sea-level. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 07, 1962
- Accession Number
- AD0413437
Entities
People
- D.d. Brewer
- J.h. Adams
Organizations
- Boeing