Payload deployment from launch vehicle using canted springs for

Details Payload deployment from launch vehicle using canted springs for Payload deployment from launch vehicle using canted springs for

1982-05-18

1985-03-26

Barefoot, Galen L.

Aeronautics and astronautics

Spacecraft

Spacecraft formation, orbit, or interplanetary path

244161, 244137R, 89 15F, 124 16, B64G 164

Patent

active

045068526

ABSTRACT:
An apparatus for launching a payload, such as a spacecraft or satellite, from a launch vehicle in which a single instrumentality is employed to simultaneously impart angular momentum about the center of mass of the payload and linear momentum in a direction along the axis of rotation.

REFERENCES:
patent: 2946151 (1960-07-01), Traylor et al.
patent: 3191342 (1965-06-01), Chalmers
patent: 3380687 (1968-04-01), Wrench et al.
patent: 3420470 (1969-01-01), Meyer
patent: 3760730 (1973-09-01), Osborn et al.
patent: 3949518 (1976-04-01), Lenza
patent: 4015507 (1977-04-01), Toy et al.
patent: 4067308 (1978-01-01), Anderson et al.
patent: 4181062 (1980-01-01), Bernstein et al.
Wheelon, "The Impact of Space Shuttle on the Future of Communication Sat.", Nov. 9, 1978.

Affiliated with

Also associated with

Rating

Payload deployment from launch vehicle using canted springs for does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Payload deployment from launch vehicle using canted springs for , we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Payload deployment from launch vehicle using canted springs for will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1290523