Safran PPS-1350-E Hall thruster
Safran's PPS-1350-E is a materially distinct PPS-1350 Hall-thruster variant. Safran's datasheet specifies 2.5 kW nominal power, 140 mN thrust, and 1,800 s specific impulse for the E configuration; an ESA system study identifies nominal and redundant PPS1350-E units in a spacecraft propulsion architecture. The bounded sources establish the variant and application without asserting a current production lifecycle.
Identity
- Aliases
- PPS®1350-EPPS1350-E
- Domains
- spaceflight
- Identity Level
- variant
- Kind
- electric-thruster
- Name
- Safran PPS-1350-E Hall thruster
- Status
- unknown
Details
- Description
- Safran's PPS-1350-E is a materially distinct PPS-1350 Hall-thruster variant. Safran's datasheet specifies 2.5 kW nominal power, 140 mN thrust, and 1,800 s specific impulse for the E configuration; an ESA system study identifies nominal and redundant PPS1350-E units in a spacecraft propulsion architecture. The bounded sources establish the variant and application without asserting a current production lifecycle.
- Electric Specs
- Input Power Max
- …
- Input Power Min
- …
- Specific Impulse Max
- …
- Specific Impulse Min
- …
- Thrust Max
- …
- Thrust Min
- …
- Propellants
- xenon
Links
Assets & Meta
- Creation Time
- August 15, 2026 at 03:06:52 UTC
- Updated Time
- August 15, 2026 at 03:06:52 UTC
Other
- Sources
- Accessed Date
- 2026-08-14
- Note
- Safran's PPS1350 datasheet distinguishes the PPS1350-S and PPS1350-E configurations and specifies PPS1350-E at 2,500 W, 140 mN, and 1,800 s with xenon propellant.
- Publisher
- Safran Spacecraft Propulsion
- Title
- PPS1350 Spacecraft Propulsion Datasheet
- Accessed Date
- 2026-08-14
- Note
- ESA's CDF study identifies one nominal and one redundant PPS1350-E Hall-effect thruster in the studied spacecraft propulsion architecture, providing an application boundary for the variant.
- Publisher
- European Space Agency
- Title
- CDF Study Report SPP NEO