CubeSat - Model MPS-120 - High-Impulse Adaptable Modular Propulsion System
From Space and Launch Systems- Space Propulsion Systems- CubeSat
MPS-120 CubeSat High-Impulse Adaptable Modular Propulsion System (CHAMPS) is a 1U hydrazine propulsion system that provides both primary propulsion and 3-axis control capabilities in a single package. The system is designed for CubeSat customers needing significant ΔV capabilities including constellation deployment, orbit maintenance, attitude control, momentum management, and de-orbit.
Specifications and Performance
Specifications and Performance
- Dimensions: 10cm x 10cm x 11.35cm
- Mass: <1.3 kg Dry, <1.6 kg Wet
- Operational Temperature Range: +5°C to +50°C
- Command Method: Digital or Discreet Analog 5V
- Power Consumption: <4W Startup, <1W Operation
- Operational Voltage: 5V Nominal
- BOL Thrust: 2.79N (high thrust) to 0.26N (low thrust) per thruster
- Minimum Impulse Bit (at blowdown-averaged feed pressure): 0.00484 to 0.000467 N-sec per thruster
22 CFR 125.4(b)(13) applicable
Development Status
In Development
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