GATE Jetpack
GATE Space
GATE Jetpack is a plug-and-play chemical propulsion module for ESPA-class satellites, providing orbit transfer, attitude control, collision avoidance, refueling support and deorbit capability.
Key figurescomparable across the catalogue
- Mass
- 36 kg
- Payload capacity
- 100 kg
- Thrust
- 1 N
- Specific impulse
- 270 s
- Total impulse
- 36,000 N·s
- Lead time
- 9 months
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Total impulse (Jetpack S)
- 36,000 Ns
- Lead time (Jetpack S)
- 9 months
- Thrusters (Jetpack S)
- 4 × [1 – 6 N]
- Thrust modes (Jetpack S)
- Continuous — Pulsed — Cold gas — Deep throttling 1:10
- Propellants (Jetpack S)
- C2H6 and N2O
- Specific impulse (Jetpack S)
- 270 s
- Module mass (Jetpack S)
- 36 kg
- Module dimensions (Jetpack S)
- 525 × 525 × 380 mm
- Payload mass (Jetpack S)
- 100 kg
- Payload/deployer dimensions (Jetpack S)
- 600 × 600 × 600 mm
- Delta-v (Jetpack S)
- 300 m/s
- Separation ring size (Jetpack S)
- 15 inch
- Rideshare port (Jetpack S)
- Rideshare ½ port
- Starlink port (Jetpack S)
- Starlink ½ port (or larger)
- Total impulse (Jetpack 80,000 Ns variant)
- 80,000 Ns
- Lead time (Jetpack 80,000 Ns variant)
- 9 months
- Thrusters (Jetpack 80,000 Ns variant)
- 4 × [20 N]
- Propellants (Jetpack 80,000 Ns variant)
- C2H6 and N2O
- Specific impulse (Jetpack 80,000 Ns variant)
- 270 s – 300 s
- Module mass (Jetpack 80,000 Ns variant)
- 80 kg
- Module dimensions (Jetpack 80,000 Ns variant)
- 800 × 800 × 400 mm
- Payload mass (Jetpack 80,000 Ns variant)
- 100 kg / 200 kg
- Payload/deployer dimensions (Jetpack 80,000 Ns variant)
- 690 × 690 × 690 mm
- Delta-v (Jetpack 80,000 Ns variant)
- 500 m/s / 300 m/s
- Separation ring size (Jetpack 80,000 Ns variant)
- 15 or 24 inch
- Rideshare port (Jetpack 80,000 Ns variant)
- Rideshare full port
- Starlink port (Jetpack 80,000 Ns variant)
- Starlink full port (or larger)
- Total impulse (Jetpack 140,000 Ns variant)
- 140,000 Ns
- Lead time (Jetpack 140,000 Ns variant)
- 9 months
- Thrusters (Jetpack 140,000 Ns variant)
- 4 × [20 N]
- Propellants (Jetpack 140,000 Ns variant)
- C2H6 and N2O
- Specific impulse (Jetpack 140,000 Ns variant)
- 270 s – 300 s
- Module mass (Jetpack 140,000 Ns variant)
- 105 kg
- Module dimensions (Jetpack 140,000 Ns variant)
- 900 × 900 × 400 mm
- Payload mass (Jetpack 140,000 Ns variant)
- 200 kg
- Payload/deployer dimensions (Jetpack 140,000 Ns variant)
- 990 × 990 × 990 mm
- Delta-v (Jetpack 140,000 Ns variant)
- 500 m/s
- Separation ring size (Jetpack 140,000 Ns variant)
- 24 inch
- Rideshare port (Jetpack 140,000 Ns variant)
- Rideshare full port XL
- Starlink port (Jetpack 140,000 Ns variant)
- Starlink full port (or larger)
About
The GATE Jetpack is a high-thrust chemical propulsion system from Gate Space, built for satellites, capsules and landing vehicles. It uses long-duration, storable propellants (C2H6 ethane and N2O nitrous oxide) fed through 4 thrusters to enable fast orbit transfers, mission reconfigurations, collision avoidance maneuvers, in-orbit refueling, and safe deorbiting. The system is designed with a plug-and-play form factor that integrates smoothly into ESPA-class satellites, minimizing development effort, reducing integration time and cost, and accelerating time to space. Its modular, efficient architecture is engineered for scalability, suitable for a single spacecraft or a full constellation, offering an affordable path to extend satellite capabilities. Thrusters support continuous, pulsed, cold-gas, and deep-throttling (1:10) operating modes. The Jetpack is offered in three sizes with total impulse ranging from 36,000 Ns up to 140,000 Ns, module masses from 36 kg to 105 kg, and support for payload masses from 100 kg to 200 kg, delivering delta-v from 300 m/s up to 500 m/s depending on configuration. It mounts via 15-inch or 24-inch separation systems compatible with Rideshare and Starlink half/full deployer ports (or larger). Lead time is approximately 9 months, with pricing starting at €450,000 for the smallest variant. Development is backed by years of hands-on rocket engine experience, including over 8,000 cold-flow and hot-fire tests across various propulsion system configurations.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.