NanoACE
CubeSat technology demonstration
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
- ^ 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.
- v
- t
- e
- Shijian 13
- Cygnus CRS OA-7 , (ALTAIR , CXBN-2 , IceCube , SG-Sat , SHARC)
- Soyuz MS-04
- Tianzhou 1, SilkRoad-1
- USA-276 / NROL-76
- Koreasat 7, SGDC-1
- GSAT 9 / South Asia Satellite
- Inmarsat-5 F4
- SES-15
- "It's a Test"
- EKS-2
- QZS-2
- ViaSat-2, Eutelsat 172B
- Dragon CRS-11 (NICER, BRAC Onnesha, GhanaSat-1, Mazaalai, Nigeria EduSat-1)
- GSAT-19
- EchoStar 21
- Progress MS-06
- HXMT / Insight, ÑuSat 3
- ChinaSat 9A
- Cartosat-2E, Max Valier Sat, Aalto-1, Blue Diamond, Green Diamond, Red Diamond, CICERO-6, COMPASS-2, InflateSail, Lemur-2 × 8, LituanicaSAT-2, ROBUSTA-1B
- Kosmos 2519 / Nivelir, Kosmos 2521 / Sputnik Inspektor
- BulgariaSat-1
- Iridium NEXT × 10
- EuropaSat / Hellas Sat 3, GSAT-17
- Shijian-18†
- Intelsat 35e
- Kanopus-V-IK, Flying Laptop, Flock-2k × 48, Landmapper BC 1, Landmapper BC 2, Lemur-2 × 8
- Soyuz MS-05
- OPTSAT-3000, VENµS
- Dragon CRS-12, ASTERIA
- Blagovest 11L
- TDRS-M
- Michibiki 3
- Formosat-5
- ORS-5
- IRNSS-1H
- USA-277 / OTV-5
- Amazonas 5
- Soyuz MS-06
- Kosmos 2522 / GLONASS-M 752
- USA-278 / NROL-42
- AsiaSat 9
- Yaogan-30-01 × 3
- Intelsat 37e, BSAT-4a
- VRSS-2
- Iridium NEXT × 10
- QZS-4
- SES-11 / EchoStar 105
- Sentinel-5 Precursor
- Progress MS-07
- USA-279 / Quasar 21
- Koreasat 5A
- SkySat × 6 , Flock-3m × 4
- BeiDou-3 M1, BeiDou-3 M2
- Mohammed VI-A
- Cygnus CRS OA-8E (Asgardia-1, EcAMSat, Lemur-2 × 8, TechEdSat-6)
- Fengyun-3D
- NOAA-20
- Jilin-1 Video × 3
- Yaogan-30-02 (3 satellites)
- Meteor-M No.2-1, Landmapper BC 3, Lemur-2 × 10
- Kosmos 2524
- LKW-1
- Alcomsat-1
- Galileo FOC 15-18
- Dragon CRS-13
- Soyuz MS-07
- GCOM-C, SLATS
- Iridium NEXT 31–40
- Yaogan-30-03 × 3
- AngoSat 1
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).