SSLV-D1
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The SSLV-D1 was the first mission of the
Small Satellite Launch Vehicle The Small Satellite Launch Vehicle (SSLV) is a small-lift launch vehicle developed by the Indian Space Research Organisation (ISRO) to deliver payload to low Earth orbit () or payload to Sun-synchronous orbit (). The rocket supports multi-or ...
(SSLV). Due to a sensor fault during separation of second stage and subsequent initiation of Open Loop Guidance by onboard computer to salvage the mission, the upper stage did not fire for planned duration and payloads were ultimately injected into a decaying orbit not achieving the objectives of mission.


Details

ISRO developed a small satellite launch vehicle (SSLV) to cater the launch of up to 500 kg satellites to Low Earth Orbits on ‘launch-on-demand’ basis. SSLV-D1 mission launched EOS 02, a 135 kg satellite, with a planned
Low Earth orbit A low Earth orbit (LEO) is an geocentric orbit, orbit around Earth with a orbital period, period of 128 minutes or less (making at least 11.25 orbits per day) and an orbital eccentricity, eccentricity less than 0.25. Most of the artificial object ...
of about 350 km altitude, at an inclination of about 37 degrees. EOS-02 was an Earth observation satellite designed and realised by ISRO. This microsat-type satellite offered advanced optical
remote sensing Remote sensing is the acquisition of information about an physical object, object or phenomenon without making physical contact with the object, in contrast to in situ or on-site observation. The term is applied especially to acquiring inform ...
operating in infrared band with high spatial resolution. The bus configuration was derived from IMS-1 bus. The mission also carried the AzaadiSAT satellite. AzaadiSAT was a 8U Cubesat weighing around 8 kg. It carried 75 different payloads each weighing around 50 grams and conducting femto-experiments. Girl students from rural regions across the country were provided guidance to build these payloads. The payloads were integrated by the student team of “Space Kidz India”. The payloads included a UHF-VHF Transponder working in ham radio frequency to enable voice and data transmission for amateur radio operators, a solid state PIN diode-based Radiation counter to measure the ionising radiation in its orbit, a long-range transponder and a selfie camera. The ground system developed by ‘Space Kidz India’ was to be utilised for receiving the data from this satellite.


Launch

SSLV launched on its maiden flight at 03:48
UTC Coordinated Universal Time (UTC) is the primary time standard globally used to regulate clocks and time. It establishes a reference for the current time, forming the basis for civil time and time zones. UTC facilitates international communica ...
/ 09:18
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on 7 August 2022, from the
First Launch Pad Satish Dhawan Space Centre – SDSC (formerly Sriharikota Range – SHAR) is the primary spaceport of the Indian Space Research Organisation (ISRO), located in Sriharikota, Tirupati district, Andhra Pradesh. The spaceport is located on an isla ...
, but failed to reach the intended orbit. Due to an anomaly detected with accelerometers after second stage separation the stage as well as the two satellite payloads were injected into an unstable elliptical orbit measuring 356km × 76km and subsequently destroyed upon reentry. According to the ISRO, the mission software failed to identify and correct a sensor fault and switched to Open Loop Guidance to salvage the mission. This led to the VTM stage firing only briefly (0.1s) and payloads were injected to a very low perigee.


References

{{Reflist ISRO space launch vehicles Small Satellite Launch Vehicle