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A Review Paper on the History and the Construction of Cryogenic Engine

Author(s):

Himanshu Shivcharan Bhandare , Raisoni

Keywords:

Liquid Propellant and Oxidizer, Newtons 3rd Law of Motion, Cryogenic Temperature, Rocket Engine

Abstract

Cryogenic is technology that every country wanted but due to its complex working and difficulty of handling of liquid propellant and oxidizer make it hard to develop. Only few countries have achieve and master this technology. Cryogenic engine follows the newtons third law of motion i.e; there is always equal and opposite reaction. Cryogenic engines have more efficiency than solid and liquid propellant. Every engine work only when it losses its heat but the whole concept of this engine is to loss heat and get output in the form of thrust. Nominal thrust of cryogenic engine is about 196.5 KN in vacuum with the specific impulse of 434 sec. All the cryogenic engine available follow some cycle for the operation basically there are four cycles which have discovered. Every engine have the basic component only difference in those engine are the flow of the fuel and the oxidizer in the engine. This technology is important because of that MTCR (Missile Technology Control Regime) restrict the use of cryogenic engine for missile manufacturing.

Other Details

Paper ID: IJSRDV7I40888
Published in: Volume : 7, Issue : 4
Publication Date: 01/07/2019
Page(s): 747-751

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