Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path
Reexamination Certificate
2005-01-25
2005-01-25
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Spacecraft
Spacecraft formation, orbit, or interplanetary path
C244S118100
Reexamination Certificate
active
06845949
ABSTRACT:
A system for providing an interface between a launch vehicle and a payload of the launch vehicle includes payload integration points of the launch vehicle that remain unchanged relative to different payload configurations, such that a payload is configurable apart from the launch vehicle. The system makes it possible to de-couple payload installation and launch vehicle turnaround operations. Payloads can be configured off-line from launch vehicle processing, thus making it possible to accommodate unique payloads while reducing wear and tear on the launch vehicle.
REFERENCES:
patent: 4044974 (1977-08-01), Lingley et al.
patent: 4290570 (1981-09-01), Smolik et al.
patent: 4303214 (1981-12-01), Wittmann et al.
patent: 4324374 (1982-04-01), Wittmann et al.
patent: 4359201 (1982-11-01), Thomson et al.
patent: 4395005 (1983-07-01), Ganssle
patent: 4646994 (1987-03-01), Petersen et al.
patent: 4711417 (1987-12-01), Steffy
patent: 4771971 (1988-09-01), Ludwig et al.
patent: 4776539 (1988-10-01), Byers et al.
patent: 4789118 (1988-12-01), Byers
patent: 4860974 (1989-08-01), Barnett et al.
patent: 5411226 (1995-05-01), Jones et al.
patent: 5848766 (1998-12-01), Thompson
patent: WO 8605158 (1986-09-01), None
CCT Project Spotlight,Command and Control Technologies Corporation; http://www.ptvs.cctcorp.com; Apr. 2001; 2 pgs.
http://science.ksc.nasa.gov/shuttle/technology/sts-newsref/spacelab.html; 15 pgs; Information content from the NSTS Shuttle Reference Manual (1988) Last Hypertexed Thursday Aug. 31, 2000.
Blackwell-Thompson Judith C.
Gale Anita E.
Graves John A.
Dinh Tien
Harness & Dickey & Pierce P.L.C.
The Boeing Company
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