1 / 11

The Small Payload Quick Return System (SPQR) As A Testbed for Future Planetary Probe Missions

The Small Payload Quick Return System (SPQR) As A Testbed for Future Planetary Probe Missions June 22, 2012. Marcus S. Murbach (POC) NASA Ames Research Center [ marcus.s.murbach@nasa.gov ] 650-604-3155 510 290 3158 (cell). Introduction. Projected future upmass capability.

ivan
Download Presentation

The Small Payload Quick Return System (SPQR) As A Testbed for Future Planetary Probe Missions

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. The Small Payload Quick Return System (SPQR) As A Testbed for Future Planetary Probe Missions June 22, 2012 Marcus S. Murbach (POC) NASA Ames Research Center [marcus.s.murbach@nasa.gov] 650-604-3155 510 290 3158 (cell)

  2. Introduction Projected future upmass capability Projected future downmass capability

  3. Hot gas de-orbit system Corona style re-entry vehicle

  4. Drag-assisted techniques Sample De-orbit with β=1 (Jacchia-Roberts Atmospheric Model)

  5. SPQR – Small Payload Quick Return SPQR concept of operations

  6. Cold gas ISS payload return system Earlier ISS Cold-gas Sample Return Capsule (SRC study)

  7. SPQR – Small Payload Quick Return Sample SPQR Altitude vs. Orbit/Time Plot

  8. TDRV – Tube Deployed Re-entry Vehicle TDRV deployment TDRV on board camera view Deployment 134km May 2009

  9. The SPQR cannister Phase Change Thermal Control Unit integrated module (model)

  10. Propulsive and Other De-orbit Options Cygnus Piggy Back concept(courtesy Orbital Sciences Corp.) Cold gas concept

  11. Atromos Mars 2-point Network

More Related