100 mN Thruster - ECAPS - SmallSat Catalog - Orbital Transports
Additional Information
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)
Documentation
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. 
 

100 mN HPGP Thruster

ECAPS
Description
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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Additional Information
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)
Documentation
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.