Adjustable heat rejection system

Details Adjustable heat rejection system Adjustable heat rejection system

1995-12-22

1998-03-31

Flanigan, Allen J.

Heat exchange

With vehicle feature

165 86, B64G 150

Patent

active

057327653

ABSTRACT:
A spacecraft having a spacecraft body and a heat radiator attached to the spacecraft body. The heat radiator is in thermal contact with the spacecraft body and the heat radiator moves from an initial position to a deployed position where heat is emitted therefrom. The predetermined deployed position is located at an angular position .theta. as measured relative to the initial position, wherein .theta. ranges from approximately 135.degree. to less than 180.degree..

REFERENCES:
patent: 3260305 (1966-07-01), Leonard et al.
patent: 3563307 (1971-02-01), Paine
patent: 4561614 (1985-12-01), Olikara et al.
patent: 4738304 (1988-04-01), Chalmers et al.
patent: 5027892 (1991-07-01), Bannon et al.
patent: 5356095 (1994-10-01), Aker

Affiliated with

Also associated with

Rating

Adjustable heat rejection system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Adjustable heat rejection system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Adjustable heat rejection system will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-44391