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IAI Beresheet

Spacecraft and Launch Vehicles

IAI Beresheet was a demonstrator of a small robotic lunar lander and lunar probe, co-developed by SpaceIL and Israel Aerospace Industries with support from the Israel Space Agency and its major financier Morris Kahn. It was the first privately initiated Moon mission and was stimulated by the Google Lunar X Prize. The lander stood about 1.5 metres high, had a net mass of 150 kilograms and about 585 kilograms when fuelled at launch. Its propulsion system was designed and built by Israel Aerospace Industries and used monomethylhydrazine fuel with mixed oxides of nitrogen oxidizer, with a restartable main engine called the LEROS 2b. It launched on 22 February 2019 on a SpaceX Falcon 9 as a secondary payload, was captured into lunar orbit on 4 April 2019, and crashed on the Moon on 11 April 2019 after a gyroscope failure during the landing approach.

Facts
Year
2019 1
Propulsion
Monomethylhydrazine and mixed oxides of nitrogen 2
Engine Class
Rocket 2
Status
Destroyed 2
Mass (kg)
150 2
Comparison
Body Style
Spacecraft 1
Connections

Exemplifies

Space Transport, Modes
Source Beresheet (Wikipedia)

Of Make

Source Beresheet (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Beresheet (Wikipedia)Planning and construction
Quote, Planning and construction
Beresheet was co-developed by SpaceIL and Israel Aerospace Industries (IAI)

Originated In

Also in Geography Atlas: where this subject originated.

Source Beresheet (Wikipedia)Planning and construction
Quote, Planning and construction
Beresheet was co-developed by SpaceIL and Israel Aerospace Industries (IAI)
Sources
1. GlobalSecurity.org: Beresheet lunar lander
GlobalSecurity.org
  • Lead
    launched from Cape Canaveral on board of a Space-X Falcon 9 rocket on 22 February 2019
  • Lead, body style
    is the Israeli lunar lander
View the Source
2. Beresheet (Wikipedia)
  • Lead
    which resulted in the lander crashing on the Moon
  • Propulsion
    the main engine was the LEROS 2b liquid-propellant, restartable rocket engine
  • Lead, net mass
    Its net mass was 150 kg (330 lb)
  • Planning and construction
    Beresheet was co-developed by SpaceIL and Israel Aerospace Industries (IAI)
  • Propulsion, propulsion
    based on monomethylhydrazine (MMH) fuel and mixed oxides of nitrogen (MON) oxidizer
View the Source
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