Names | Fast, Affordable, Science and Technology Satellite-Huntsville 01 FASTSAT-HSV 01 FASTSAT-Huntsville 01 USA-220 |
---|---|
Mission type | Technology demonstration |
Operator | NASA / MSFC |
COSPAR ID | 2010-062D |
SATCAT no. | 37225 |
Mission duration | 2 years (planned) 13 years, 8 months, 20 days (in orbit) |
Spacecraft properties | |
Manufacturer | NASA Marshall Space Flight Center [1] |
Launch mass | 180 kg (400 lb) |
Dimensions | 61 × 71 × 97 cm (24 × 28 × 38 in) |
Power | 90 watts |
Start of mission | |
Launch date | 20 November 2010, 01:25:00 UTC |
Rocket | Minotaur IV / HAPS |
Launch site | Kodiak Launch Complex, Pad 1 |
Contractor | Orbital Sciences |
Entered service | 2010 |
Orbital parameters | |
Reference system | Geocentric orbit [2] |
Regime | Low Earth orbit |
Perigee altitude | 626 km (389 mi) |
Apogee altitude | 653 km (406 mi) |
Inclination | 72.0° |
Period | 97.7 minutes |
Fast, Affordable, Science and Technology Satellite-Huntsville 01 or FASTSAT-Huntsville 01 of the NASA. FASTSAT-HSV 01 was flying on the STP-S26 mission - a joint activity between NASA and the U.S. Department of Defense Space Test Program, or DoD STP. FASTSAT and all of its six experiments flying on the STP-S26 multi-spacecraft/payload mission have been approved by the Department of Defense Space and Experiments Review Board (USA-220). [1]
The satellite was designed, developed and tested over a period of 14 months at NASA's Marshall Space Flight Center in Huntsville, Alabama, in partnership with the Von Braun Center for Science & Innovation and Dynetics, both of Huntsville, and the Department of Defense's Space Test Program. [1]
FASTSAT HSV-01, a microsatellite satellite bus that carried six experiment payloads to low Earth orbit. There were six experiments (3 NASA, 3 DoD), including: [1]
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