The Shavit, Hebrew for comet, is the small satellite launch vehicle that Israel has flown since 1988 to place reconnaissance satellites in low Earth orbit. Development began in 1982 under the general management of Israel Aircraft Industries, and it first flew on 19 September 1988 with the Ofek-1 satellite, which made Israel the eighth nation with an orbital launch capability. It is a three-stage solid-propellant rocket with an optional liquid-fuel fourth stage, and its first two stages were taken from the Jericho II missile. Hostile neighbours lie to the east, so it is launched westward from Palmachim Airbase over the Mediterranean into retrograde orbits, which lowers the payload it can carry. It had flown 13 times, reaching orbit 11 times, with failures on the fourth and sixth flights, the second of which destroyed the Ofek 6 satellite in September 2004. South Africa produced a licensed version called the RSA-3.
Facts
SignificanceIsraeli satellite launcher derived from the Jericho II missile and essentially identical to the South African RSA-3 2 Engine Class Maximum Mass (kg) Connections
Exemplifies
Source Shavit 2 (Wikipedia)
Of Make
Source Shavit 2 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Shavit 2 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
is manufactured by Israel Aircraft Industries (IAI)
Originated In
Also in Geography Atlas: where this subject originated.
Source Shavit 2 (Wikipedia)Lead, body styleQuote, Lead, body style
is a small lift launch vehicle produced by Israel from 1982 onwards
Sources
1. Shavit 2 (Wikipedia)
Lead
It was first launched on 19 September 1988
Lead, body style
is a small lift launch vehicle produced by Israel from 1982 onwards
Lead, engine class
The launcher consists of three stages powered by solid-fuel rocket motors, with an optional liquid-fuel fourth stage
Lead, manufacturer
is manufactured by Israel Aircraft Industries (IAI)
View the Source2. Encyclopedia Astronautica: Shavit
Encyclopedia AstronauticaEncyclopedia entry
Satellite launcher derived from Jericho II MRBM, essentially identical to South African RSA-3.
Key facts
Gross mass 23,630 kg (52,090 lb)
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