The present invention is directed to a multifunction structure (MFS) in which electrical/electronic componentry, thermal control and structural support are integrated into a monolithic structure that is particularly useful in spacecraft applications. The multifunctional structure is also designed to be modular so that the electrical/electronic componentry can be repaired or replaced.
申请公布号
WO9925165(A2)
申请公布日期
1999.05.20
申请号
WO1998US23840
申请日期
1998.11.06
申请人
LOCKHEED MARTIN CORPORATION;BARNETT, DAVID, M.;RAWAL, SURAJ, P.;MORGENTHALER, DANIEL, R.;HARRIS, EDWARD, N.
发明人
BARNETT, DAVID, M.;RAWAL, SURAJ, P.;MORGENTHALER, DANIEL, R.;HARRIS, EDWARD, N.