22 N HPGP Thruster
ECAPS
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The 100 mN HPGP thruster is a compact, non-toxic propulsion system designed for small satellites and CubeSats. This enables high thrust apogee, reaction control and proximity operations maneuvering for satellites.
The thruster operates on LMP-103S low-toxicity monopropellant with 1.3X the density-Isp of hydrazine. Additionally, LMP-103S offers up to 72%(1) cheaper spacecraft loading as compared to hydrazine, reducing the total life-cycle cost of the mission. The Propellant is long term storable (>15 years) and enables "fuel at the factory" for rapid response satellites.
| Parameter | Value |
|---|---|
| Thrust Range | 30 to 100 mN |
| Propellant | LMP-103S |
| Mass | 0.04 (excluding Flow Control Valve) |
| Length | 55 mm (excluding Flow Control Valve) |
| Flow Control Valve Type | Solenoid |
| Pull-in Voltage | 10 (+/-2.5) VDC |
| Holding Voltage | 3.3 VDC |
| Nominal Reactor Pre-heating Voltage | 9 VDC |
| Regulated Reactor Pre-heating Power | 6.3 to 8 W |
| Minimum Impulse Bit | < 5 mNs |
| Pulses | 2000 (qualification level) |
| Propellant Throughput | 1 Kg (qualification level) |
| Longest Continuous Firing Time | 18 minutes (qualification level) |
| Accumulated Firing Time | 3.0 hrs (qualification level) |
| Firing Sequences | 180 (qualification level) |
The 100 mN HPGP thruster is a compact, non-toxic propulsion system designed for small satellites and CubeSats. This enables high thrust apogee, reaction control and proximity operations maneuvering for satellites.
The thruster operates on LMP-103S low-toxicity monopropellant with 1.3X the density-Isp of hydrazine. Additionally, LMP-103S offers up to 72%(1) cheaper spacecraft loading as compared to hydrazine, reducing the total life-cycle cost of the mission. The Propellant is long term storable (>15 years) and enables "fuel at the factory" for rapid response satellites.
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