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13 relations: CE-7.5, Cryogenic rocket engine, Gas-generator cycle, Geosynchronous Satellite Launch Vehicle Mark III, GSAT-14, Hindustan Aeronautics Limited, India, Indian Space Research Organisation, Liquid hydrogen, Liquid oxygen, Liquid Propulsion Systems Centre, Specific impulse, Thrust-to-weight ratio.
CE-7.5
The CE-7.5 is a cryogenic rocket engine developed by the Indian Space Research Organisation to power the upper stage of its GSLV Mk-2 launch vehicle.
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Cryogenic rocket engine
A cryogenic rocket engine is a rocket engine that uses a cryogenic fuel or oxidizer, that is, its fuel or oxidizer (or both) are gases liquefied and stored at very low temperatures.
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Gas-generator cycle
The gas-generator cycle is a power cycle of a bipropellant rocket engine.
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Geosynchronous Satellite Launch Vehicle Mark III
The Geosynchronous Satellite Launch Vehicle Mark III (GSLV-III), also referred to as the Launch Vehicle Mark 3 (LVM3) is a three-stage medium-lift launch vehicle developed by the Indian Space Research Organisation (ISRO).
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GSAT-14
GSAT-14 is an Indian communications satellite launched in January 2014.
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Hindustan Aeronautics Limited
Hindustan Aeronautics Limited (HAL) is an Indian state-owned aerospace and defence company headquartered in Bangalore, India.
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India
India (IAST), also called the Republic of India (IAST), is a country in South Asia.
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Indian Space Research Organisation
The Indian Space Research Organisation (ISRO) is the space agency of the Government of India headquartered in the city of Bangalore.
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Liquid hydrogen
Liquid hydrogen (LH2 or LH2) is the liquid state of the element hydrogen.
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Liquid oxygen
Liquid oxygen—abbreviated LOx, LOX or Lox in the aerospace, submarine and gas industries—is one of the physical forms of elemental oxygen.
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Liquid Propulsion Systems Centre
The Liquid Propulsion Systems Centre (LPSC) is a research and development centre functioning under Indian Space Research Organisation.
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Specific impulse
Specific impulse (usually abbreviated Isp) is a measure of how effectively a rocket uses propellant or jet engine uses fuel.
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Thrust-to-weight ratio
Thrust-to-weight ratio is a dimensionless ratio of thrust to weight of a rocket, jet engine, propeller engine, or a vehicle propelled by such an engine that indicates the performance of the engine or vehicle.
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