Rohini
Credit: ISRC
Indian earth land resources satellite. 2 launches, 1980.07.18 (Rohini RS-1) and 1983.04.17 (Rohini 3). Experimental-technology mission.
Gross mass: 41 kg (90 lb).
First Launch: 1980.07.18.
Last Launch: 1983.04.17.
Number: 2 .
More... - Chronology...
Associated Countries
See also
Associated Launch Vehicles
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SLV Indian all-solid orbital launch vehicle. More...
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SLV-3 Indian all-solid orbital launch vehicle. Four stage vehicle consisting of 1 x SLV-3-1 + 1 x SLV-3-2 + 1 x SLV-3-3 + 1 x SLV-3-4 More...
Associated Manufacturers and Agencies
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ISRO Indian manufacturer of rockets, spacecraft, and rocket engines. Indian Space Research Organization, India. More...
Bibliography
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McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
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JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: here.
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McDowell, Jonathan, Launch Log, October 1998. Web Address when accessed: here.
Associated Launch Sites
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Sriharikota India's primary space launch center, located on the east coast of the peninsula with a firing sector over the Bay of Bengal. In use from 1971 to present. More...
Rohini Chronology
1980 July 18 - .
02:33 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLV.
LV Family:
SLV.
Launch Vehicle:
SLV-3.
LV Configuration: SLV-3 SLV-3-E2.
- Rohini RS-1 - .
Payload: Rohini 1B. Mass: 40 kg (88 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: Rohini. Decay Date: 1981-05-20 . USAF Sat Cat: 11899 . COSPAR: 1980-062A. Apogee: 921 km (572 mi). Perigee: 307 km (190 mi). Inclination: 44.7000 deg. Period: 97.00 min. Summary: Experimental-technology mission. Rohini satellite RS-1. .
1983 April 17 - .
05:44 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLV.
LV Family:
SLV.
Launch Vehicle:
SLV-3.
LV Configuration: SLV-3-D4 SLV-3-D4.
- Rohini 3 - .
Payload: Rohini RS-D-2. Mass: 42 kg (92 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: Rohini. Decay Date: 1990-04-19 . USAF Sat Cat: 14002 . COSPAR: 1983-033A. Apogee: 485 km (301 mi). Perigee: 326 km (202 mi). Inclination: 46.6000 deg. Period: 92.70 min. Summary: Rohini satellite D-2. Second developmental flight of an SLV-3 launch vehicle. The Rohini satellite D-2 carried a sensor payload for conducting remote-sensing experiments and for accurate orbit and attitude determination. .
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