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13 relations: CE-20, Cryogenic rocket engine, Geosynchronous Satellite Launch Vehicle, GSAT-14, Hindustan Aeronautics Limited, India, Indian Space Research Organisation, KVD-1, Liquid hydrogen, Liquid oxygen, Liquid Propulsion Systems Centre, Rocket engine, Staged combustion cycle.
CE-20
The CE-20 is a cryogenic rocket engine developed by the Liquid Propulsion Systems Centre, a subsidiary of Indian Space Research Organisation.
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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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Geosynchronous Satellite Launch Vehicle
Geosynchronous Satellite Launch Vehicle abbreviated as GSLV, is an expendable launch system operated 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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KVD-1
KVD-1 was an upper stage LOX/LH2 cryogenic engine developed by Isayev Design Bureau (now KB KhIMMASH) of Russia in early 1960s.
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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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Rocket engine
A rocket engine uses stored rocket propellant mass for forming its high-speed propulsive jet.
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Staged combustion cycle
The staged combustion cycle (sometimes known as topping cycle or preburner cycle) is a power cycle of a bipropellant rocket engine.
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