Hyperenvironment Simulation.Part II. Development And Design Of Simulation Facilities For Space And Vehicle Environment
Report Number: WADD TR 60-785 Part II
Author(s): McCoy, T. M.
Corporate Author(s): Northrop Corporation
Laboratory: Flight and Engineering Test Group
Date of Publication: 1960-12
Pages: 93
Contract: AF 33(616)-6679
DoD Project: 1309
DoD Task: 13000
Identifier: AD0257775
AD Number: AD257775
Abstract:
This report summarizes the approach, concept, design, and cost of hyperenvironmental simulation facilities for evaluating effects of space vehicle environment on specimens up to 250 pounds are summarized. With the objective of combining environment variables wherever applicable and feasible, four basic facilities were conceived with several environments each. Detailed design specifications for these facilities are contained under separate covers. As part of the design back-up, some of the problems, methods and techniques of simulation are discussed. A summary is also given of the pertinent results of some experiments conducted to prove design feasibility in certain critical areas of simulation.
Provenance: Bombardier/Aero
Author(s): McCoy, T. M.
Corporate Author(s): Northrop Corporation
Laboratory: Flight and Engineering Test Group
Date of Publication: 1960-12
Pages: 93
Contract: AF 33(616)-6679
DoD Project: 1309
DoD Task: 13000
Identifier: AD0257775
AD Number: AD257775
Abstract:
This report summarizes the approach, concept, design, and cost of hyperenvironmental simulation facilities for evaluating effects of space vehicle environment on specimens up to 250 pounds are summarized. With the objective of combining environment variables wherever applicable and feasible, four basic facilities were conceived with several environments each. Detailed design specifications for these facilities are contained under separate covers. As part of the design back-up, some of the problems, methods and techniques of simulation are discussed. A summary is also given of the pertinent results of some experiments conducted to prove design feasibility in certain critical areas of simulation.
Provenance: Bombardier/Aero