scholarly journals Solar Orbiter: Mission and spacecraft design

Author(s):  
C. García Marirrodriga ◽  
A. Pacros ◽  
S. Strandmoe ◽  
C. Ashcroft ◽  
C. Damasio ◽  
...  
2010 ◽  
Vol 150 (1-4) ◽  
pp. 23-62 ◽  
Author(s):  
Craig R. Tooley ◽  
Martin B. Houghton ◽  
Richard S. Saylor ◽  
Cathy Peddie ◽  
David F. Everett ◽  
...  

Author(s):  
Craig R. Tooley ◽  
Martin B. Houghton ◽  
Richard S. Saylor ◽  
Cathy Peddie ◽  
David F. Everett ◽  
...  

Author(s):  
Bernhard Geiger ◽  
Alejandro Cardesin Moinelo ◽  
David Frew ◽  
Mike Ashman ◽  
Juan Jose Garcia Beteta ◽  
...  
Keyword(s):  

Author(s):  
James E. Graf ◽  
Richard W. Zurek ◽  
James K. Erickson ◽  
Benhan Jai ◽  
M.D. Johnston ◽  
...  
Keyword(s):  

2018 ◽  
pp. 72-78
Author(s):  
A. V. Gorbunov ◽  
Yu. A. Zhukov ◽  
E. V. Korotkov ◽  
A. V. Lekanov ◽  
V. G. Porpylev ◽  
...  

The vast majority of electronic devices on-Board Russian spacecraft is placed on a temperature-controlled mounting surface is ON, however, in some tasks there is a necessity to place a separate electronic units out thermostated panels on remote spacecraft design. The article presents an autonomous system of providing thermal regime of electronic blocks of spacecraft and objects of space technology that require maintaining the operating temperature and are unable to be installed on the thermostatic landing surfaces of spacecraft. The proposed autonomous system of providing thermal regime can operate autonomously in the extended operating temperature range of the installation surface from -80 to +80 °C when the supply voltage changes in the range from 75 to 550% of the nominal value. The review of the existing solutions is presented, the substantiation of the proposed decision is given, the structural scheme of autonomous system of providing thermal regime is given and its description and an example of application is given.


2007 ◽  
Vol 02 (01) ◽  
pp. 27-34 ◽  
Author(s):  
Sachit Butail ◽  
Mason Peck
Keyword(s):  

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