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Rohini Satellite RS-1Series Launched by Indian launch vehicle SLV-3 First RS-1 Launch Date: July 18, 1980 Weight: 35 kg Orbit: 300 km x 900 km elliptical orbit 97 minutes period Lauched by:. SLV-3 launched with Rohini Technology Payload from SLV LP, Satish Dhawan Space Centre, India on Friday Aug 10, 1979 at 02:28 UTC. The first launch of an orbital class rocket which was designed and built by India. It failed to. Email this Article. Series of Indian technology test and earth land resources satellite. Technology satellite for ISRO, India. Launched 1979-1980. Technology satellite for ISRO, India. Launched 1979-1980. Details about satellite, networks, hacking and general knowledge etc. And clarify the doubts and helps for all visitors and users and followers.

Rohini Manufacturer ISRO Country of origin India Operator ISRO Applications Experimental Satellites Specifications Design life 8 Launch mass 30–41.5 kilograms 66–91 lb Dimensions 360 Power 3 watts RTP 16 watts others. 2015/07/04 · Satellite Launch Vehicle SLV was India's first rocket. A four stage, all solid rocket, it could carry a 40 Kg payload to orbit. The first experimental flight of SLV-3, in August 1979, was only.

Rohini Satellites RS: Rohini-I RS-I was the first Indan satellite launched from Sriharikota by India’s own launch vehicle, SLV-3 in 1980. Its main objective was to evaluate the performance of the fourth stage of SLV-3 launch vehicle and monitor important parameters such as velocity, separation shock, pressures and temperatures. Rohini satellites were experimental satellites. i.e., there primary mission was for ISRO to learn satellite and launch vehicle technologies Eg: telemetry, tracking, stabilization, remote sensing etc., rather than any specific “real world. Rohini RS-D2 ര ഹ ണ എന നത ഇന ത യ സ പ സ റ സ ച ച ഓ ഗന സ ഷ അയച ച ഉപഗ രഹശ ര ണ യ ട പ ര ണ. ര ഹ ണ ശ ര ണ യ 4 ഉപഗ രഹങ ങ ആണ ണ ട യ ര ന നത. Rohini Technology Payload [1] It was a 35 Kg experimental spin stabilised satellite that used 3W of power and was launched on 1979-08-10 from SDSC.The satellite contained instruments to monitor the launch vehicle. [2] It did not [3.

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