Cold Ammonia Corrective Propulsion System

Purpose:
Corrective propulsion system (CPS) is intended for correction and stabilization of orbit parameters and zeroing of the kinetic moment of flywheel engines in the spacecraft orientation system.
Year of release: 2014
Guaranteed service life (years): 5
Estimated production / delivery time (months): 12
Flight qualification of the product: Да
Brief history of flight qualification:
Components in the spacecraft "Meteor" and "Electro".
Possibility to adapt the product to customer requirements: Да


Parameter Value
Total thrust 5000…5500 N×s
Engine thrust 0,02…0,8 N
Weight of CPS Not more than 17 kg
CPS power consumption at impulse output No more than 50 W
CPS working body ammonia

Description

Corrective propulsion system is an installation which includes such components as: a working fluid tank with a film electric heater, a receiver, a steam generator, a valve with an integrated micro nozzle.

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