NanoACE
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Mission type | Technology demonstration |
---|---|
Operator | Terran Orbital[1] |
COSPAR ID | 2017-042V |
Website | tyvak.eu/missions/nanoace |
Spacecraft properties | |
Spacecraft type | CubeSat (3U)[2] |
Manufacturer | Tyvak Nano-Satellite Systems |
Launch mass | 5.2 kg (11 lb)[1] |
Dimensions | 30 cm × 10 cm × 10 cm (11.8 in × 3.9 in × 3.9 in)[2] |
Power | 4 deployable solar panels |
Start of mission | |
Launch date | July 14, 2017, 7:36am UTC[3] |
Rocket | Soyuz-2.1a |
Launch site | Baikonur Cosmodrome |
Contractor | Roscosmos |
Orbital parameters | |
Regime | Low Earth Orbit[4] |
Periapsis altitude | 566.9 km (352.3 mi)[5] |
Apoapsis altitude | 581.5 km (361.3 mi)[5] |
Inclination | 97.4°[5] |
Period | 96 minuets[5] |
NanoACE is a technology demonstration CubeSat by Tyvak Nano-Satellite Systems to validate their communications, navigation, guidance, and software technology.[1][6] NanoACE was launched onboard a Soyuz-2.1a Fregat-M, on July 14, 2017, along with Russian Earth imaging satellite Kanopus-V-IK and 71 other CubeSats.[7]
The satellite has two Infrared and two visible light cameras.[6] It can maneuver via its cold gas propulsion system.[2][6]
References
[edit]- ^ a b c "NANOACE". tyvak.eu. Tyvak Nano-Satellite Systems, Inc. 2017. Retrieved January 29, 2024.
- ^ a b c Krebs, Gunter (2023). "NanoACE". space.skyrocket.de. Gunter's Space Page. Retrieved January 29, 2024.
- ^ Foust, Jeff (2017). "Soyuz Launches 73 satellites". spacenews.com. SpaceNews. Retrieved January 29, 2024.
- ^ Burger, Edward; Bordacchini, Giulia (2019). Yearbook on Space Policy 2017. Cham, Switzerland: Springer. p. 321. ISBN 978-3-030-05417-5.
- ^ a b c d "NANOACE". n2yo.com. Retrieved February 2, 2024.
- ^ a b c "NanoACE". spaceflight101.com. Spaceflight101. 2017. Retrieved February 2, 2024.
- ^ Werner, Debra (2017). "Astro Digital announces first cubesats launched on Soyuz failed". spacenews.com. SpaceNews. Retrieved February 2, 2024.