ISO after completing its successful mission

Cryogenics

Volumn 39, Issue 2, 1999, Pages 135-148

  Seidel, Albert ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ASTRONOMICAL SATELLITES; CRYOGENIC EQUIPMENT; INSTRUMENT TESTING; SERVICE LIFE; SPACE APPLICATIONS; SUPERFLUID HELIUM; TEMPERATURE; THERMAL LOAD;

CRYOSTAT VACUUM VESSEL TEMPERATURE; INFRARED SPACE OBSERVATORY; PAYLOAD MODULE;

CRYOSTATS;

EID: 0033359283     PISSN: 00112275     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0011-2275(99)00009-0     Document Type: Article

References (4)

1. Seidel A., Wanner M., Davidson M. The current ISO-cryostat design. Proc ICEC. 12:1988;669-675.
2. Seidel A., Paßvogel Th. The ISO-cryostat; It's qualification status. Adv Cryog Engin. 37B:1991;1327-1340.
3. Paßvogel Th, Seidel A, Wilz E, Sagner U. The design and testing of the ISO-PLM, 24th ICES-Conference, 20-23 June 1994, SAE-paper 941274.
4. Jochimsen G. Simulation of fluid behaviour by lumped masses in the ISO-Payload Module, ESA-Conference on Spacecraft Structures, Materials and Mechanical Testing, Noordwijk, Netherlands, 27-30 March 1996.