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Concept
Bipropellant System
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Summary
A
Bipropellant System
is a
Rocket propulsion system
that uses two separate propellants, a fuel and an oxidizer, which are stored in
Separate tanks
and mixed in a
Combustion Chamber
to
Produce thrust
. This type of system allows for more efficient and
Powerful propulsion
compared to
Monopropellant systems
, making it ideal for
High-performance space missions
.
Concepts
Rocket Propulsion
Combustion Chamber
Fuel
Oxidizer
Thrust
Specific Impulse
Propellant Tanks
Liquid Propellant
Hypergolic Propellant
Cryogenic Propellant
Rocket Engine
Liquid Rocket Engine
Relevant Degrees
Air and Space Transport Engineering 100%
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