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词条 Satellite Launch Vehicle
释义

  1. Launch History

  2. See also

  3. References

{{about|the Indian launch vehicle|the term "Satellite launch vehicle"|Launch vehicle}}{{Infobox Rocket
|image = SatLaunchVehicle.jpeg
|caption = Satellite Launch Vehicle Source ISRO
|imsize = 80px
|height = {{convert|22|m|ft|abbr=on}}
|mass = {{convert|17000|kg|lb|abbr=on}}
|diameter = {{convert|1|m|ft|abbr=on}}
|manufacturer = ISRO
|function = Small launch vehicle
|country-origin = India
|capacities =
|location = 400km LEO
|kilos = {{convert|40|kg|lb|abbr=on}}
|status = Retired
|first = 10 August 1979
|last = 17 April 1983
|launches = 4
|success = 2
|fail = 1
|partial = 1
|sites = Sriharikota
|derivatives = ASLV, PSLV
|payloads = Rohini
|stagedata =
|type = stage
|stageno = First
|engines = 1 solid
|SI = 253 sec
|burntime = 49 seconds
|fuel = PBAN (Polybutadine Acrylo Nitrate) Solid[1]
|propmass = 8.6 tonnes
|thrust = 46 tonnes
  }}   {{Infobox Rocket/Stage

|type = stage
|stageno = Second
|engines = 1 solid
|SI = 267 sec
|burntime = 40 seconds
|fuel = PBAN (Polybutadine Acrylo Nitrate)Solid
|propmass = 3 tonnes
|thrust = 20 tonnes
  }}   {{Infobox Rocket/Stage

|type = stage
|stageno = Third
|engines = 1 solid
|SI = 277 sec
|burntime = 45 seconds
|fuel = high energy propellant (HEF 20)Solid
|propmass = 1 tonnes
|thrust = 6.3 tonnes
  }}   {{Infobox Rocket/Stage

|type = stage
|stageno = Fourth
|engines = 1 solid
|SI = 283 sec
|burntime = 33 seconds
|fuel = high energy propellant (HEF 20)Solid
|propmass = 262 kg
|thrust = 2.4 tonnes
}}

The Satellite Launch Vehicle (Hindi: उपग्रह प्रक्षेपण यान), or SLV was a 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 {{Nowrap|{{convert|400|km}}}} and carry a payload of {{nobreak|{{cvt|40|kg}}}}.[2] The first experimental flight of SLV-3, 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 statistics ==

{{ #invoke:Chart | bar chart
| float = center
| width = 400
| height = 300
| stack = 1
| group 1 = 1:0:0:0:0
| group 2 = 0:0:1:0:0
| group 3 = 0:1:0:0:1
| colors = FireBrick : Orange: ForestGreen
| group names = Failure : Partial failure : Success
| units suffix = _launches
| x legends = 1979 : 1980 : 1981: 1982: 1983
}}

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.[6]

Flight №Date / time (UTC)Rocket,
Configuration
Launch sitePayloadPayload massOrbitUserLaunch
outcome
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