PROGRAM 461 RELIABILITY LIFE TEST VEHICLE 0007
Abstract
Contents: Environmental Test Facility; Vacuum chamber, End closures, Feedthroughs, Vacuum cham ber instrumentation and control, Description of chamber operation, Vacuum system and equipment, Thermal simulation system, Selecting the system, HIVOS orbital simulation system, Thermal sink, Simulation of solar and terrestrial radiation, Heat flux simulator control system, Radiometers, Radiometer and reflector cooling system, Test equipment, Automatic programming and test system, Low speed data system (LOSDAS), Communication and control system, Programmed automatic system timer, Test director's console, and Calibration. Facility Test Equipment Performance; Performance summary, Description of operation conditions, Vacuum chamber, Heat flux simulator, and Automatic test equipment.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 30, 1963
- Accession Number
- AD0417756
Entities
Organizations
- Lockheed Martin Missiles and Space