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  • 1
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    Satellite retrieval and servicing operations with proximity operations modules (1982)
    In:  CASI
    Details
    Publication Date: 2006-04-12
    Description: The concept of manned and unmanned proximity modules (POM) to assist the Orbiter in retrieval, servicing, and emergency operations of orbiting payloads is discussed. An unmanned POM, capable of examining or capturing and returning to the Orbiter large satellites which are station-keeping at distances up to one kilometer from the Orbiter, is presented and its design features defined. Also presented is the concept of a manned POM which is capable of capturing and maneuvering smaller payloads in or about the Orbiter payload bay. The manned POM also serves as a free flying work station used to support satellite servicing and provide a back-up to Orbiter situations when the remote manipulator is inoperative.
    Keywords: SPACE TRANSPORTATION
    Type: NASA. Johnson Space Center Satellite Serv. Workshop, Vol. 2; 21 p
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Satellite services and orbital retrieval (1985)
    In:  CASI
    Details
    Publication Date: 2006-02-14
    Description: Within the capabilities of the Space Shuttle Orbiter, a broad range of services which can be made available to the satellite user community as summarized. Payload deployment, close proximity retrieval, and a number of other mission related functions are discussed. The focus here is on close proximity retrieval and retrieval of payloads in higher energy low Earth orbits.
    Keywords: LAUNCH VEHICLES AND SPACE VEHICLES
    Type: NASA. Lyndon B. Johnson Space Center Orbital Debris; p 299-315
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Satellite power system LEO vs GEO assembly issues (1977)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: A strawman crystal-silicon 5-GW Satellite Power System (SPS) concept formed the basis of a study of construction concepts for building a complete SPS in low earth orbit (LEO) or geosynchronous orbit (GEO). Construction scenarios were evolved, including factory-in-space concepts and operations. Design implications imposed on the SPS satellite as a consequence of in-orbit assembly operations, and related attitude control requirements during assembly in LEO or GEO environments, were also evaluated. Results are presented indicating that complete assembly of an operational SPS in LEO, followed by transport to GEO, does not appear technically desirable. The best mix, however, of LEO versus GEO construction activity remains to be resolved.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: AIAA PAPER 77-1029 , Conference on New options in energy technology; Aug 02, 1977 - Aug 04, 1977; San Francisco, CA
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Manual lunar orbit rendezvous analysis. (1967)
    In:  Other Sources
    Details
    Publication Date: 2019-06-27
    Description: Lunar Module rendezvous with Command and Service Modules in lunar orbit, discussing thrusting-maneuver schedule
    Keywords: SPACE VEHICLES
    Format: text
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    NASA TECHNICAL REPORTS
  • 5
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    Report of the Transportation Panel (1985)
    In:  CASI
    Details
    Publication Date: 2019-08-13
    Description: Tether applications for space transportation are covered: (1) payload boast; (2) upper stage boost; (3) E.T. deboost; (4) shuttle deboost; (5) shuttle docking ; (6) payload and OTV boost; (7) OTV payload boost; (8) lunar assist and eccentricity change; (9) aeromaneuvering by remote sail or kite; (10) electrodynamic deceleration; and (11) lunar and planetary applications. The first seven transfer momentum between two masses at the tether tips, and the remaining for use tethers for controlled interaction with the environment.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Appl. of Tethers in Space, Vol. 2; 56 p
    Format: text
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    NASA TECHNICAL REPORTS
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