Small lift launch vehicle produced by Israel from 1982 onwards
For the village in Iran sometimes Romanized as "Shavit", see Shavi, Dezful.
Shavit 2 שביט
Function
Expendable launch vehicle
Manufacturer
Israel Aerospace Industries
Country of origin
Israel
Cost per launch
$18M
Size
Height
26.4 m
Diameter
1.35 m
Mass
30,500–70,000 kg
Stages
4
Capacity
Payload to LEO
Mass
350–800 kg [1]
Launch history
Status
Active
Launch sites
Palmachim Airbase
Total launches
12
Success(es)
10
Failure(s)
2
First flight
19 September 1988
Last flight
28 March 2023
First stage (LeoLink LK-1) – LK-1
Powered by
LK-1
Maximum thrust
553.8 kN (124,499 lbf)
Specific impulse
268 seconds
Burn time
55 seconds
Propellant
HTPB
First stage (LeoLink LK-2) – Castor 120
Maximum thrust
1650.2 kN (370,990 lbf)
Specific impulse
280 seconds
Burn time
82 seconds
Propellant
HTPB polymer, Class 1.3 C
Second stage – LK-1
Powered by
1 LK-1
Maximum thrust
515.8 kN
Specific impulse
268 seconds
Burn time
55 seconds
Propellant
HTPB
Third stage – RSA-3-3
Powered by
1 RSA-3-3
Maximum thrust
58.6 kN
Specific impulse
298 seconds
Burn time
94 seconds
Propellant
Solid
Fourth stage – LK-4
Powered by
1 LK-4
Maximum thrust
0.402 kN
Specific impulse
200 seconds
Burn time
800 seconds
Propellant
Hydrazine[2]
[edit on Wikidata]
Shavit 2 (Hebrew: "comet" – שביט) is a small lift launch vehicle produced by Israel from 1982 onwards, to launch satellites into low Earth orbit. It was first launched on 19 September 1988 (carrying an Ofek-1 satellite payload), making Israel the eighth nation to have an orbital launch capability[3] after the USSR, United States, France, Japan, People's Republic of China, United Kingdom, and India.
The Shavit 2 project is believed to have been an offshoot development, resulting from Israel's Jericho nuclear armed intercontinental ballistic missile (ICBM) program.[4][5]
Shavit rockets are launched from Palmachim Airbase by the Israel Space Agency into highly retrograde orbits over the Mediterranean Sea to prevent debris coming down in populated areas and also to avoid flying over nations hostile to Israel to the east; this results in a lower payload-to-orbit than east-directed launches would allow.[3][6] The launcher consists of three stages powered by solid-fuel rocket motors, with an optional liquid-fuel fourth stage, and is manufactured by Israel Aircraft Industries (IAI).
The Republic of South Africa produced and tested a licensed version in cooperation with Israel called the RSA-3 in an ultimately unsuccessful bid to produce a domestic satellite launch vehicle and ballistic missile; the South African program was closed in 1994.[7]
An earlier unrelated project called Shavit 2 was the first Israeli sounding rocket, launched on 5 July 1961 for meteorological research.[8] Shavit Three, with an altitude reported as 100 miles (160 km), was launched on 11 August 1961.
^"Shavit", Space launch systems, Deagel
^"Astronautix leolinklk-1 Review". Archived from the original on 28 December 2016. Retrieved 14 June 2021.
^ ab"Shavit". Space Launch Report. 20 April 2014. Archived from the original on 25 January 2016. Retrieved 7 July 2015.{{cite web}}: CS1 maint: unfit URL (link)
^"Delivery systems", Israel (country profile), NTI.
^Report of the Secretary-General (1991). South Africa's Nuclear-Tipped Ballistic Missile Capability(PDF). Department for Disarmament Affairs. Disarmament Study Series. New York: United Nations. doi:10.18356/8afa8632-en. ISBN 92-1-142178-0.
^Stephen Clark (22 June 2010). "New Israeli spy satellite blasts off into the night". Spaceflight Now. Retrieved 7 July 2015.
^"RSA". Archived from the original on 3 March 2016. Retrieved 6 February 2015.
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