Satellite Launch Vehicle

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Satellite Launch Vehicle
FunctionSmall-lift launch vehicle
ManufacturerISRO
Country of originIndia
Size
Height22 m (72 ft)
Diameter1 m (3.3 ft)
Mass17,000 kg (37,000 lb)
Capacity
Payload to LEO
Altitude400 km (250 mi)
Mass40 kg (88 lb)
Associated rockets
Derivative work
Solid

The Satellite Launch Vehicle or SLV was a

Indian Space Research Organisation to develop the technology needed to launch satellites. SLV was intended to reach a height of 400 kilometres (250 mi) and carry a payload of 40 kg (88 lb).[2] The first experimental flight of SLV, in August 1979, was a failure.[3]
The first successful launch took place on 18 July 1980.

It was a four-stage rocket with all solid-propellant motors.[3]

The first launch of the SLV took place in Sriharikota on 10 August 1979. The fourth and final launch of the SLV took place on 17 April 1983.

It has taken approximately seven years to realise the vehicle from start. The solid motor case for first and second stage are fabricated from 15 CDV6 steel sheets and third and fourth stages from fibre reinforced plastic.[1]

Launch history

All four SLV launches occurred from the

SLV Launch Pad at the Sriharikota High Altitude Range. The first two launches were experimental (E) and the next 2 were designated as developmental (D) as this was the first launch vehicle being developed by India not intended for a long service life.[4]

Flight No. Date / time (UTC) Rocket,
Configuration
Launch site Payload Payload mass Orbit User Launch
outcome
E1 10 August 1979 Satellite Launch Vehicle
SLV Launch Pad
Rohini Technology Payload[5] 35 kg
Low Earth
ISRO Failure
Faulty valve caused vehicle to crash into the Bay of Bengal 317 seconds after launch.[4]
E2 18 July 1980 Satellite Launch Vehicle
SLV Launch Pad
Rohini RS-1
35 kg
Low Earth
ISRO Success [4]
It was the first satellite successfully launched by the indigenous launch vehicle SLV. It provided data on the fourth stage of SLV.
D1 31 May 1981 Satellite Launch Vehicle
SLV Launch Pad
Rohini RS-D1 38 kg
Low Earth
ISRO Partial failure
Orbit too low. Decayed after 9 days[4]
D2 17 April 1983 Satellite Launch Vehicle
SLV Launch Pad
Rohini RS-D2 41.5 kg
Low Earth
ISRO Success[4]
Earth Observation satellite

Launch statistics

1
1979
1980
1981
1982
1983
  •   Failure
  •   Partial failure
  •   Success
Decade-wise summary of SLV launches
Decade Successful Partial success Failure Total
1970s 0 0 1 1
1980s 2 1 0 3
Total 2 1 1 4

See also

References

  1. ^ a b "First Successful Launch of SLV-3 - Silver Jubilee" (PDF). ISRO. Archived from the original (PDF) on 12 November 2020. Retrieved 11 February 2019.
  2. ^ "Launch Vehicles". Department of Space, Government of India. Archived from the original on 1 February 2014. Retrieved 19 January 2014.
  3. ^ a b "SLV". isro.gov.in. Archived from the original on 29 May 2017. Retrieved 5 September 2015.
  4. ^ a b c d e TS Subramanian. "Silver jubilee of the first successful SLV-3". Frontiline. Archived from the original on 8 February 2018. Retrieved 8 February 2018.
  5. ^ "Rohini Technology Payload". Archived from the original on 31 July 2017. Retrieved 28 December 2014.