Engineering:Small Payload Quick Return
Small Payload Quick Return (SPQR) is a NASA Ames Research Center concept to return small payloads from orbit.[1]
The system uses an Exo-Brake, a parachute-like drag device for use in the low-pressure exosphere of Low Earth Orbit. This is the first part of a three part return system, operating from 350 to 100 km.[2]
Exo-Brake
The first test of the Exo-Brake system from orbit began with the launching of the TechEdSat-3p nano-satellite from the International Space Station on November 19, 2013.[3]
TechEdSat-4 is expected to test an Exo-Brake with variable drag in 2014.[3]
TechEdSat-3p took over 60 days to deorbit, while TechEdSat-4 reentered in about 30 days.[4]:Fig 3
A newer Exo-Brake system was tested on TechEdSat-5, deployed from the ISS in 2017.[5] It is a flexible cross shape that can be warped for steering during reentry.[5]
SOAREX Flights
Several investigations related to the SPQR programs and TechEdSat have been flown on Sub-Orbital Aerodynamic Re-entry Experiments (SOAREX) sounding rockets flights.
SOAREX-6 flew 27 November 2008 on an ATK Sub-orbital/Orion 50xl sounding rocket.
SOAREX-7 flew 28 May 2009 aboard a Terrier-Orion sounding rocket launched from Wallops Flight Facility (WFF) in Virginia. A TDRV (Tube Deployed Re-entry Vehicle) was successfully tested after the flight reached its apogee of 134 km.[6]
On SOAREX-8, which launched on a Terrier Black-Brant suborbital sounding rocket, a wireless sensor module, a camera, various communication devices, and a full Exo-Brake were tested.
On SOAREX-9, a wireless sensor module, a camera, and various communication devices were tested.[7]
References
- ↑ Characterizing An Experimental Decelerator For Delivering Nano-Sat Payloads To Planetary Surfaces Kevin Ramus et al., U. of Idaho, [1]
- ↑ The SPQR as an Option for Returning Payloads from the ISS after the Termination of STS Flights Marcus Murbach et al., NASA Ames Research Center, [2]
- ↑ 3.0 3.1 Exo-Brake Parachute Launched From International Space Station by Keith Cowling, SpaceRef, Nov 2013 [3]
- ↑ "TechEdSat-4 (Technological and Educational Nanosatellite-4) - Satellite Missions - eoPortal Directory". https://directory.eoportal.org/web/eoportal/satellite-missions/content/-/article/techedsat-4.
- ↑ 5.0 5.1 "Exo-Brake Enables Safe Return for Small Spacecraft - Tech Briefs :: Aerospace & Defense Technology". April 2017. https://www.aerodefensetech.com/component/content/article/tb/techbriefs/machinery-and-automation/26698.
- ↑ Murbach, M. S. (15 June 2015). "n Overview of the SOAREX" and" TechEdSat Flight Series: Missions To Advance Re-entry Experimentation, Planetary Mission Design," and" Flight Technology". Koln, Germany: NASA. https://solarsystem.nasa.gov/docs/1_04_An%20Overview%20of%20the%20SOAREX%20and%20TechEdSat%20Flight%20Series_M.S.%20Murbach.pdf.
- ↑ Murbach, Marcus. "TechEdSat 5 / PhoneSat 5 (T5/P5) SmallSat Presentation 2016". https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3490&context=smallsat.
 |  |
