Cold Gas Reaction Control Systems

Nitrogen cold gas thruster modules from 0.01 N to 5 N for precision attitude manoeuvring on cubesat and small satellite platforms. Inert propellant — no handling restrictions.

Cold gas reaction control system thruster cluster assembly for spacecraft
Technical Specifications

CG-Series Performance Parameters

CG-50 (Standard Module)

ParameterValue
Thrust (nominal)0.5 N
Thrust range0.05 – 1.0 N
Specific Impulse68 s (GN₂, 200 bar)
PropellantGaseous Nitrogen (GN₂)
Tank Pressure100 – 300 bar
Min. Impulse Bit0.0005 N·s
Valve Response< 3 ms
Mass (module)0.085 kg
Envelope45 × 45 × 60 mm
QualificationECSS-E-ST-35C Level 1

CG-200 (High-Thrust)

ParameterValue
Thrust (nominal)5 N
Thrust range0.5 – 5 N
Specific Impulse72 s (GN₂, 250 bar)
PropellantGaseous Nitrogen (GN₂)
Tank Pressure150 – 350 bar
Min. Impulse Bit0.005 N·s
Valve Response< 4 ms
Mass (module)0.24 kg
Envelope70 × 70 × 90 mm
QualificationECSS-E-ST-35C Level 1
Applications

Platform Compatibility

Design Drivers

Cubesat & Small Sat Constraints

Mass and volume budgets are tight. Propellant handling restrictions apply in integration facilities. Mission operators require predictable, characterised impulse bits for ADCS algorithms.

  • 6U–16U cubesat volume envelopes
  • No toxic propellant authorisation in many facilities
  • Digital valve control from ADCS board
  • Thermal compatibility with CubeSat Standard
CG-Series Solution

Compact, Safe, Characterised

Inert GN₂ propellant with no ADR or special handling. Miniaturised solenoid valve with sub-3 ms response. Standard RS-422 digital interface. Impulse bit characterisation data supplied with each unit.

  • CG-50 integrates in 6U cubesat propulsion bay
  • COTS GN₂ cartridges available (optional)
  • Pre-characterised impulse bit tables
  • Operating temperature: -60 °C to +80 °C

Request CG-Series Datasheet

Full qualification test reports, impulse bit characterisation data, and interface documentation available for qualified programmes.