Effectiveness and Value of Space Vehicle Thermal Vacuum Testing

2020 ◽  
Vol 63 (1) ◽  
pp. 63-74
Author(s):  
John W. Welch ◽  
Bailey Z. Zhao ◽  
Derek J. McVay

Abstract Environmental testing of spacecraft flight hardware is performed to detect design and workmanship defects and verify mission requirements prior to launch. At the space vehicle level of assembly, the thermal vacuum test simulates an environment particularly well-suited for verifying mission performance requirements. In this paper, the test objectives of the space vehicle thermal vacuum test are reviewed and an assessment is made of the effectiveness and value of the test. Recent thermal vacuum test data is used to determine how the uniqueness of the thermal vacuum test environment achieves test purposes and how the test ensures mission assurance for space vehicles.

1988 ◽  
Vol 31 (6) ◽  
pp. 30-38
Author(s):  
Elhanan Dgany ◽  
Eytan Kochavi ◽  
Shimon Gruntman ◽  
Asher Kinan

A thermal vacuum testing facility for electronic units has been specified, designed, and built. It is fully operational and performs its tasks—thermal vacuum qualification and acceptance testing of electronic units. All performance requirements and design details have been carefully evaluated on a cost-effective basis, resulting in achieving the design goal of low price (purchase, operation, and maintenance) together with ease of operation, maintenance simplicity, and upgrading options. The major cost saving originated from a detailed analysis of thermal vacuum requirements that resulted in low cost substitutes to the common thermal shroud, together with a thermal plate. The plate is actively thermally controlled by a circulating fluid that is temperature regulated by a commercial heating and cooling unit. The high vacuum pumping system includes a diffusion pump with backstreaming holders.


1988 ◽  
Vol 31 (4) ◽  
pp. 26-48
Author(s):  
Arthur Jackola ◽  
John Allen

Rockwell International's Multi-Environment Test System (METS) is an environmental simulation facility for thermal cycle and thermal vacuum testing of space vehicle subsystems. The use of a central cryopump and eight radially mounted, independently controlled, test chambers provide test efficiencies not possible in single chamber test systems. Thermal cycle and thermal vacuum testing can be performed in each chamber and thereby further increase the efficiency of the test system. This article describes the Multi-Environment Test System and its configuration and control system and summarizes its use to support black-box environmental test programs.


2000 ◽  
Author(s):  
M. Marchesi ◽  
R. Campaci ◽  
A. Nista ◽  
W. Prendin ◽  
S. Scarpa ◽  
...  

2008 ◽  
Author(s):  
Shiro Ueno ◽  
Dmitry Khrustalev ◽  
Peter Cologer ◽  
Russ Snyder

1996 ◽  
Author(s):  
K. Miller Hurlbert ◽  
M. K. Ewert ◽  
J. Graf ◽  
J. Keller ◽  
K. A. Pauley
Keyword(s):  

Author(s):  
A. G. Vikulov

We implemented a systemic scientific approach to thermal vacuum development of spacecraft, which integrates the problems of thermal calculations, thermal vacuum tests and accuracy evaluation for mathematical models of heat transfer by means of solving identification problems. As a result, the following factors increase the efficiency of spacecraft ground testing: reducing the duration of thermal vacuum tests, making autonomous thermal vacuum testing of components possible, increasing the accuracy of thermal calculations


Author(s):  
Do-Hyeong Kim ◽  
Yeon-Hwang Jeong ◽  
Gyeong-Mo Tak ◽  
Jun-Ho Lee ◽  
Won-Ho Cha ◽  
...  
Keyword(s):  

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