Astronomy:Team Miles
| Mission type | Technology demonstration |
|---|---|
| Website | team |
| Mission duration | 2 years and 5 days (in orbit) |
| Spacecraft properties | |
| Spacecraft | Team Miles |
| Spacecraft type | CubeSat |
| Bus | 6U CubeSat |
| Manufacturer | Fluid and Reason, LLC. |
| Launch mass | 14 kg (31 lb) |
| Dimensions | 10 cm × 20 cm × 30 cm |
| Start of mission | |
| Launch date | 16 November 2022, 06:47:44 UTC[1] |
| Rocket | SLS Block 1 |
| Launch site | KSC, LC-39B |
| Contractor | NASA |
| Orbital parameters | |
| Reference system | Heliocentric orbit |
| Flyby of Moon | |
| Transponders | |
| Band | S-band |
NASA CubeQuest Challenge | |
Team Miles was a 6U CubeSat that was to demonstrate navigation in deep space using innovative plasma thrusters. It was also to test a software-defined radio operating in the S-band for communications from about 4 million kilometers from Earth. Team Miles was one of ten CubeSats launched with the Artemis 1 mission into a heliocentric orbit in cislunar space on the maiden flight of the Space Launch System (SLS), that took place on 16 November 2022.[1][2] Team Miles was deployed but contact was not established with the spacecraft.[3]
Overview
| Parameter | Units/performance |
|---|---|
| Thrust | 5 mN |
| Specific impulse (Isp) | 760 seconds |
| Impulse | 7456 N seconds |
| Power | 22 watts |
| Wet mass | 1.5 kg |
| Propellant mass | 1 kg |
| Propellant | Solid iodine |
| Thrust:Mass | 3.3 mN/kg |
| Impulse:Power | 338 N seconds/watt |
| Delta-V 12 kg craft | 649 m/s |
The spacecraft, a 6-Unit CubeSat — measuring 10 cm × 20 cm × 30 cm — was designed and is being developed by a non-profit group of fifteen citizen scientists and engineers (Fluid and Reason, LLC) based at Tampa, Florida.[4][5][6] Since the Team Miles won the first place at CubeQuest Challenge for the selection process,[7] Fluid and Reason, LLC stroke partnerships and became Miles Space, a commercial endeavor to further develop the technology and intellectual property that has come out of the design process.[4]
Propulsion
Wesley Faler, who leads Fluid and Reason, LLC., is the inventor of the ion thruster to be used, which he calls ConstantQ Model H.[8][4] It is a form of electric propulsion for spacecraft. The engine is a hybrid plasma and laser thruster that uses ionized iodine as propellant.[9][6] The Model H system includes 4 thruster heads which are canted, allowing for both primary propulsion and attitude control (orientation) without the use of moving parts.[8][10] The goal within the CubeQest Challenge is to travel 4 million kilometers, but the team will attempt to go as far as 96 million kilometers before the end of the mission.[4]
Radio
The spacecraft will use the USRP B200mini, a software-defined radio operating in the S band for communications from about 4 million kilometers from Earth.[11]
See also
- Near-Earth Asteroid Scout by NASA was a solar sail spacecraft that was planned to encounter a near-Earth asteroid (mission failure)
- BioSentinel is an astrobiology mission
- LunIR by Lockheed Martin Space
- Lunar IceCube, by the Morehead State University
- CubeSat for Solar Particles (CuSP)
- Lunar Polar Hydrogen Mapper (LunaH-Map), designed by the Arizona State University
- EQUULEUS, submitted by JAXA and the University of Tokyo
- OMOTENASHI, submitted by JAXA, was a lunar lander (mission failure)
- ArgoMoon, designed by Argotec and coordinated by Italian Space Agency (ASI)
- Team Miles, by Fluid and Reason LLC, Tampa, Florida
- The 3 CubeSat missions removed from Artemis 1
- Lunar Flashlight will map exposed water ice on the Moon
- Cislunar Explorers, Cornell University, Ithaca, New York
- Earth Escape Explorer (CU-E3), University of Colorado Boulder
References
- ↑ 1.0 1.1 Roulette, Joey; Gorman, Steve (2022-11-16). "NASA's next-generation Artemis mission heads to moon on debut test flight" (in en). Reuters. https://www.reuters.com/lifestyle/science/nasas-artemis-moon-rocket-begins-fueling-debut-launch-2022-11-15/.
- ↑ Clark, Stephen (12 October 2021). "Adapter structure with 10 CubeSats installed on top of Artemis moon rocket". Spaceflight Now. https://spaceflightnow.com/2021/10/12/adapter-structure-with-10-cubesats-installed-on-top-of-artemis-moon-rocket/.
- ↑ "Team Miles". NASA Space Science Coordinated Archive. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=TEAMMILES.
- ↑ 4.0 4.1 4.2 4.3 "Cube Quest Challenge Spotlight: Team Miles". Space Daily. 19 May 2017. https://www.spacedaily.com/reports/Cube_Quest_Challenge_Spotlight_Team_Miles_999.html.
- ↑ Jennifer Harbaugh (18 May 2017). "Cube Quest Challenge Spotlight: Team Miles". NASA. https://www.nasa.gov/directorates/spacetech/centennial_challenges/cubequest/team_miles.
This article incorporates text from this source, which is in the public domain.
- ↑ 6.0 6.1 Jeremy S. Cook (30 August 2017). "The Miles CubeSat Might Be the Next Satellite Sent to Mars". https://www.tampabay.com/news/humaninterest/self-taught-tampa-team-poised-to-send-winning-satellite-into-deep-space/2322213.
- ↑ Roman, Monsi C.; Kim, Tony; Sudnik, Janet; Cylar, Rosalind; Porter, Molly; Sivak, Amy; Cavanaugh, Dominique; Krome, Kim (12-14 September 2017). "Centennial Challenges Program Overview: How NASA Successfully Involves the General Public in the Solving of Current Technology Gaps". AIAA SPACE and Astronautics Forum and Exposition. Orlando, Florida: AIAA Space and Astronautics Forum and Exposition. doi:10.2514/6.2017-5159. ISBN 978-1-62410-483-1. https://arc.aiaa.org/doi/pdf/10.2514/6.2017-5159. Retrieved 10 March 2021.
- ↑ 8.0 8.1 "ConstantQ Spacecraft Propulsion". Fluid and Reason, LLC.. 2017. https://fluidandreason.com/constantq/.
- ↑ Lloyd Sowers (12 May 2017). "Tampa team enters new Space Race with cube satellite". FOX13 Tampa Bay. https://www.fox13news.com/news/local-news/tampa-team-in-new-space-race.
- ↑ "ConstantQ™ Thruster". Miles Space. 2017. https://miles-space.com/thruster/.
- ↑ Scott Schaire (2018). "Investigation into New Ground Based Communications Service Offerings in Response to SmallSat Trends". 32nd Annual AIAA/USU Conference on Small Satellites Document SSC18-SI-07. https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4222&context=smallsat.
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