EO-1 Spacecraft Thermal Vacuum Testing: An Innovative Approach to Cost Effective Verification

Author(s):  
Stephen J. Krein ◽  
Nicholas M. Teti
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.


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

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):  
Henry Quach ◽  
Marcos A. Esparza ◽  
Hyukmo Kang ◽  
Aman Chandra ◽  
Heejoo Choi ◽  
...  

Proceedings ◽  
2018 ◽  
Vol 2 (8) ◽  
pp. 534
Author(s):  
Jean-François Vandenrijt ◽  
Cédric Thizy ◽  
Fabian Languy ◽  
Marc Georges

Holographic interferometry at around 10 µm wavelengths has many advantages. It offers the possibility of large deformation measurement, while being much less sensitive to external perturbations. We present the state-of-the art of this technique applied to several industrial cases of the space industry. In particular, we demonstrate that the technique is well adapted to measurement of full-field deformation maps of space structures undergoing large temperature variations typical to what they experience in space conditions.


2008 ◽  
Author(s):  
Jose I. Rodriguez ◽  
Howard Tseng ◽  
Burt Zhang ◽  
Arthur Na-Nakornpanom ◽  
Robert S. Leland

1995 ◽  
Author(s):  
Brian C. Baker ◽  
Fred E. Voss ◽  
George W. Wolfe

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