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UniSat
Unisat 6 Credit: Manufacturer Image |
Italian technology satellite developed by the GAUSS (Gruppo di Astrodinamica dell' Universita degli Studi 'la Sapienza') in Roma. Technology satellite for GAUSS (La Sapienza University of Rome), Italy. Launched 2000-2006.
Status: Operational 2000. First Launch: 2000-09-26. Last Launch: 2014-06-19. Number: 5 . Gross mass: 12 kg (26 lb).
Unisat was financed by ASI and MURST (Ministero dell'Universtia e della Ricerca Scientifica e Tecnologica). The first carried NiMH batteries, a magnetometer, and a payload consisting of a space debris sensor and a camera. Later models were used to test customer equipment and deploy cubesats or Pocket-PUCP's.
More at: UniSat.
Subtopics
| UniSat 5 Technology satellite for GAUSS Srl, Italy. Launched 2013. |
| UniSat 6 Technology satellite for GAUSS Srl, Italy. Launched 2014. |
| UniSat 7 Technology satellite for GAUSS Srl, Italy. |
Family:
Technology,
Technology satellite.
Country:
Italy.
Launch Vehicles:
R-36M 15A14,
R-36M2 15A18M,
Dnepr.
Launch Sites:
Baikonur,
Baikonur LC109.
Agency:
La Sapienza,
GAUSS.
Bibliography:
2,
552,
554.
Photo Gallery
| UniSat 1 Credit: Manufacturer Image |
| Unisat-5 Credit: Manufacturer Image |
| UniSat 7 Credit: Manufacturer Image |
2000 September 26 - .
10:05 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
Launch Pad: LC109/95.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- UniSat - .
Mass: 10 kg (22 lb). Nation: Italy.
Agency: Makeyev bureau.
Manufacturer: la Sapienza.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: UniSat.
USAF Sat Cat: 26547 . COSPAR: 2000-057C. Apogee: 670 km (416 mi). Perigee: 643 km (399 mi). Inclination: 64.56 deg. Period: 97.78 min.
Experimental satellite developed by the GAUSS (Gruppo di Astrodinamica dell' Universita degli Studi 'la Sapienza') in Roma. Unisat was financed by ASI and MURST (Ministero dell'Universtia e della Ricerca Scientifica e Tecnologica). It carried NiMH batteries, a magnetometer, and a payload consisting of a space debris sensor and a camera.
2002 December 20 - .
17:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
Launch Pad: LC109/95.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- UniSat 2 - .
Mass: 10 kg (22 lb). Nation: Italy.
Agency: Makeyev bureau.
Manufacturer: La Sapienza.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: UniSat.
USAF Sat Cat: 27608 . COSPAR: 2002-058D. Apogee: 667 km (414 mi). Perigee: 636 km (395 mi). Inclination: 64.60 deg. Period: 97.80 min.
2004 June 29 - .
06:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
Launch Pad: LC109/95.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Unisat 3 - .
Mass: 12 kg (26 lb). Nation: Italy.
Agency: La Sapienza.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: UniSat.
USAF Sat Cat: 28373 . COSPAR: 2004-025H. Apogee: 800 km (490 mi). Perigee: 684 km (425 mi). Inclination: 98.30 deg. Period: 99.80 min.
2013 November 21 - .
07:10 GMT - .
Launch Site:
Dombarovskiy.
Launch Pad: xxx.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Unisat-5 - .
Mass: 19 kg (41 lb). Nation: Italy.
Class: Technology.
Type: Technology satellite. Spacecraft: Unisat.
USAF Sat Cat: 39421 . COSPAR: 2013-066F. Apogee: 636 km (395 mi). Perigee: 592 km (367 mi). Inclination: 97.78 deg. Period: 96.97 min.
Technology satellite for the University of Rome. It carried a further eight tiny satellites within it, and one of those (PUCP-Sat) carried a further nested satellite, Pocket-PUCP. Most of the subsatellites were ejected from Unisat-5 between 08:10 and 08:25 GMT on November 21.
2014 June 19 - .
19:11 GMT - .
Launch Site:
Dombarovskiy.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Unisat 6 - .
Mass: 26 kg (57 lb). Nation: Italy.
Spacecraft: Unisat.
USAF Sat Cat: 40012 . COSPAR: 2014-033C. Apogee: 699 km (434 mi). Perigee: 613 km (380 mi). Inclination: 97.97 deg. Period: 97.86 min. Satellite by GAUSS Srl to test customer equipment and deploy four cubesats..
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