DLR-Tubsat: Difference between revisions
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{{Infobox spaceflight |
{{Infobox spaceflight |
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| name = DLR-Tubsat |
| name = DLR-Tubsat |
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| names_list = TUBSAT |
| names_list = TUBSAT-C<br>TUBSAT |
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| COSPAR_ID = 1999-029C |
| COSPAR_ID = 1999-029C |
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| SATCAT = <!--satellite catalogue number, omit leading zeroes (e.g. 25544)--> |
| SATCAT = <!--satellite catalogue number, omit leading zeroes (e.g. 25544)--> |
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| website = |
| website = |
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| mission_duration = |
| mission_duration = |
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| distance_travelled = |
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| orbit_periapsis = <!--periapsis altitude--> |
| orbit_periapsis = <!--periapsis altitude--> |
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| orbit_apoapsis = <!--apoapsis altitude--> |
| orbit_apoapsis = <!--apoapsis altitude--> |
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| orbit_inclination = 98. |
| orbit_inclination = 98.36° |
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| orbit_period = 99.24 minutes |
| orbit_period = 99.24 minutes |
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| orbit_RAAN = <!--right ascension of the ascending node--> |
| orbit_RAAN = <!--right ascension of the ascending node--> |
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| insignia_size = <!--include px/em; defaults to 180px--> |
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'''DLR-Tubsat''' ([[Pseudonym|a.k.a]] ''TUBSAT'') was a [[German]]n [[Earth observation satellite|earth observation]] [[Miniaturized satellite#Microsatellites|microsatellite]] developed in [[joint venture]] between [[Technical University of Berlin]] (TUB) and [[German Aerospace Center]] (DLR). TUB was responsible for the satellite bus and DLR was responsible for the payload.<ref name="TUBSAT">{{cite news|title=TUBSAT|publisher=eoportal.org|accessdate=9 Jul 2016|url=https://directory.eoportal.org/web/eoportal/satellite-missions/t/tubsat}}</ref> |
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Revision as of 11:07, 9 July 2016
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| Names | TUBSAT-C TUBSAT |
|---|---|
| Mission type | Experimental |
| Operator | TUB |
| COSPAR ID | 1999-029C |
| SATCAT no. | 25758 |
| Range | 713 kilometres (443 mi) |
| Apogee | 732 kilometres (455 mi) |
| Spacecraft properties | |
| Spacecraft | DLR-Tubsat |
| Manufacturer | TUB & DLR |
| Launch mass | 45 kg (99 lb) |
| Dimensions | 32 x 32 x 32 cm |
| Power | 120 W |
| Start of mission | |
| Launch date | 06:22, May 26, 1999 |
| Rocket | PSLV-C2 |
| Launch site | Sriharikota Launching Range |
| Contractor | File:ISRO Logo.gif ISRO |
| End of mission | |
| Deactivated | Not known |
| Orbital parameters | |
| Reference system | Sun-synchronous orbit |
| Regime | Low Earth orbit |
| Inclination | 98.36° |
| Period | 99.24 minutes |
DLR-Tubsat (a.k.a TUBSAT) was a Germann earth observation microsatellite developed in joint venture between Technical University of Berlin (TUB) and German Aerospace Center (DLR). TUB was responsible for the satellite bus and DLR was responsible for the payload.[1]