Thermal aspects of Hitchhiker payloads

Details Thermal aspects of Hitchhiker payloads Thermal aspects of Hitchhiker payloads

Jan 1997

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1997aipc..387..555n&link_type=abstract

Space technology and applications international forum (STAIF - 97). AIP Conference Proceedings, Volume 387, pp. 555-560 (1997).

Statistics

Applications

Spaceborne And Space Research Instruments, Apparatus, And Components, Artificial Earth Satellites, Heat Flow In Porous Media

Scientific paper

The objective of this report is to describe and discuss the thermal design, analysis and flight data of various experiments flown through the Hitchhiker (HH) Program at NASA Goddard Space Flight Center, along with a comparison study of the HH Avionics for several missions. The research entails the thermal design of the experiments, the shuttle mission profile (attitude time line) and actual flight data. One interesting flight occurred for STS-74 and the HH GLO-4/PASDE Payload (GPP). This was a MIR docking mission which required the Orbiter to fly in extreme solar inertial attitudes conducive for MIR, attitudes never flown prior to this mission. PASDE, mounted in three different bays of the Orbiter, allowed for a comparison of attitude with bay location.

Affiliated with

Also associated with

No associations

Rating

Thermal aspects of Hitchhiker payloads does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Thermal aspects of Hitchhiker payloads, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Thermal aspects of Hitchhiker payloads will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1784028