New Space Support Equipment (SSE) components developed for the Hubble Space Telescope Second Servicing Mission are described, with particular emphasis on how flight experience from the 1993 First Servicing Mission was utilized in the design and testing process. The new components include the Second Axial Carrier (SAC) Axial Scientific Instrument Protective Enclosure (ASIPE), the magnetic-damped SAC ASIPE Load Isolation System, the Enhanced Power Distribution and Switching Unit (EPDSU), and the Multi-Mission Orbital Replacement Unit Protective Enclosure (MOPE). Analytical modeling predictions are compared with on-orbit data from the Hubble Space Telescope (HST) Second Servicing Mission. Those involved in thermal designs of hardware for use on the Shuttle or Space Station, particularly with astronaut interaction, may find interest in this paper.
Thermal Design And Performance Of The Space Support Equipment For The Hubble Space Telescope Second Servicing Mission
Sae Technical Papers
International Conference On Environmental Systems ; 1997
1997-07-01
Aufsatz (Konferenz)
Englisch
Thermal Design of Space Support Equipment for the Hubble Space Telescope Servicing Mission
SAE Technical Papers | 1994
|Hubble Space Telescope Servicing Mission 3A
NTRS | 1999
Hubble Space Telescope - First Servicing Mission
NTIS | 1994
Hubble Space Telescope First Servicing Mission
SAE Technical Papers | 1994
|Hubble Space Telescope - First Servicing Mission
NTRS | 1994