Aerojet Rocketdyne, Inc.

Model MPS-130 - CubeSat High-Impulse Adaptable



MPS-130 CubeSat High-Impulse Adaptable Modular Propulsion System (CHAMPS) is a 1U AF-M315E (low-toxicity propellant) 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

  • Dimensions: 10 cm x 10 cm x 11.35 cm
  • 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: <TBD W Startup, <TBD W Operation
  • Operational Voltage: 5 V Nominal
  • BOL Thrust: TBD N (high thrust) to TBD N (low thrust) per thruster
  • Minimum Impulse Bit (at blowdown-averaged feed pressure): TBD to TBD N-sec per thruster

22 CFR 125.4(b)(13) applicable

Development Status

In Development

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