 Satellite Launch Vehicle | |
| Function | Small-lift launch vehicle |
|---|---|
| Manufacturer | ISRO |
| Country of origin | India |
| Size | |
| Height | 22 m (72 ft) |
| Diameter | 1 m (3.3 ft) |
| Mass | 17,000 kg (37,000 lb) |
| Capacity | |
| Payload to LEO | |
| Altitude | 400 km (250 mi) |
| Mass | 400 kg (880 lb) |
| Associated rockets | |
| Derivative work | ASLV, PSLV |
| Launch history | |
| Status | Retired |
| Launch sites | Satish Dhawan Space Centre |
| Total launches | 4 |
| Success(es) | 2 |
| Failure(s) | 1 |
| Partial failure(s) | 1 |
| First flight | 10 August 1979 |
| Last flight | 17 April 1983 |
| Type of passengers/cargo | Rohini |
| First stage | |
| Propellant mass | 8.6 t (19,000 lb) |
| Powered by | 1 solid |
| Maximum thrust | 450 kN (100,000 lbf) |
| Specific impulse | 253 seconds (2.48 km/s) |
| Burn time | seconds |
| Propellant | PBAN (Polybutadiene acrylonitrile) Solid[1] |
| Second stage | |
| Propellant mass | 3 tonnes |
| Powered by | 1 solid |
| Maximum thrust | 20 tonnes |
| Specific impulse | 267 sec |
| Burn time | 40 seconds |
| Propellant | PBAN (Polybutadine Acrylo Nitrate) Solid |
| Third stage | |
| Propellant mass | 1 tonnes |
| Powered by | 1 solid |
| Maximum thrust | 6.3 tonnes |
| Specific impulse | 277 sec |
| Burn time | 45 seconds |
| Propellant | High energy propellant (HEF 20) Solid |
| Fourth stage | |
| Propellant mass | 262 kg |
| Powered by | 1 solid |
| Maximum thrust | 2.4 tonnes |
| Specific impulse | 283 sec |
| Burn time | 33 seconds |
| Propellant | High energy propellant (HEF 20) Solid |
The Satellite Launch Vehicle or SLV was a small-lift launch vehicle project started in the early 1970s by the 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] The aerodynamic characterization research was conducted at the National Aerospace Laboratories' 1.2m Trisonic Wind Tunnel Facility.[4]
- ^ 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.
- ^ "Launch Vehicles". Department of Space, Government of India. Archived from the original on 1 February 2014. Retrieved 19 January 2014.
- ^ a b "SLV". isro.gov.in. Archived from the original on 29 May 2017. Retrieved 5 September 2015.
- ^ "Bengaluru: 1.2m trisonic wind tunnel at National Aerospace Laboratories completes 55 years of service". ANI. 6 June 2022. Retrieved 22 November 2024.