Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 03-May-2024

This institute began the development of a Hall effect electric propulsion motor in 1998.

-In 2001 it was already carrying out tests with this type of engines.

Hall thruster prototype
“Hall thruster prototype”

-Between 2002 and 2003, the 40 nM Hall effect model was put into operation.

-In 2004, high sustainability tests were carried out for 550 hours, in a vacuum environment.

-From then until 2008 the engines already took definitive shapes and there were convincing tests on satellites.

SISP Hall thruster
“SISP Hall thruster”

Engines of SISP

Model: Arcjet

Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: Ion thrusters

Arquitecture:
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Feed System:
Ignition:
Thrust:
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Model: Microwave plasma thrusters

Arquitecture:
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Feed System:
Ignition:
Thrust:
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Model: Propulsion elec/Hall

Arquitecture:
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Feed System:
Ignition:
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Model: Pulsed plasma thrusters

Arquitecture:
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Fuels:
Feed System:
Ignition:
Thrust:
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Model: Resistojets

Arquitecture:
Chambers:
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Feed System:
Ignition:
Thrust:
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Other details: