Safran DSI - PPS®1350 Hall Effect Thruster
The PPS®1350 Hall Effet plasma thruster draws on Safran’s long experience with electric propulsion. It is designed for orbital transfer, station keeping and deorbiting satellites and other spacecraft. In particular, the PPS 1350 was the primary engine on ESA’s lunar probe, Smart-1, launched in 2003 by an Ariane 5 rocket. This mission was completed in September 2006.
VERY HIGH PERFORMANCE
The major advantage of the PPS®1350 is of course its very high specific impulse, which allows significant weight savings versus platforms using conventional chemical propulsion. It also offers an excellent thrust-to-electrical power ratio, which enables reducing operating time or the number of thrusters needed.
IN-ORBIT EXPERIENCE
The PPS®1350 amply demonstrated its capabilities during ESA’s Smart-1 probe’s mission from Earth orbit into orbit around the Moon: 5,000 hours cumulated operating time in space Four of these thrusters handle North/South station-keeping duties on the Alphasat satellite, launched in 2013. The PPS®1350 was selected by Space Systems Loral in 2016, and will be used on the company’s communications satellites for station-keeping, and for part of the orbit-topping operation.
PPS®1350 Features
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Designed for Orbit-Topping and Station-Keeping |
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40% Weight Saving Versus Convention Propulsion |
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Excellent Thrust-to-Electrical Power Ratio |
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Safran DSI
Safran DSI Testing & Telemetry provides complete, end-to-end solutions covering instrumentation, mission systems, onboard recording, and transmission, through to base stations for data monitoring and control. Our solutions are platform-agnostic and adaptable to customer mission needs.
