AIS-SWAG2-X4 Sublimation Warm Gas Thruster
Applied Ion Systems
A next-generation quad-nozzle sublimation warm gas thruster using solid unpressurized Adamantane, providing an estimated 588uN thrust in a 92x92x67mm form factor. In development.
Technical specifications
- Type
- Sublimation Warm Gas Thruster
- Fuel
- Solid Unpressurized Adamantane
- Power
- TBD
- Thrust
- 588uN
- Operating Lifetime
- TBD
- Pre-Heat Time
- TBD
- Ramp-Up Time to Max Thrust
- TBD
- Total Impulse
- TBD
- ISP
- TBD
- Size
- 92x92x67mm
- Mass
- TBD
- Fuel Mass
- TBD
- Inputs
- 12V, 5V, GND, x1 Logic Command
- Status
- IN DEVELOPMENT
- Lead Time
- 4-6 WEEKS
About
The AIS-SWAG2-X4 is the next-generation quad-nozzle sublimation warm gas thruster at AIS, using solid unpressurized Adamantane as propellant. Housed in a 92x92x67mm form factor, the SWAG2-X4 provides an estimated 588uN of thrust — the highest thrust in the SWAG2 series. Performance specifications including total impulse, ISP, operating lifetime, and orbital movement capabilities are TBD pending development completion. The system accepts 12V, 5V, GND, and a single logic command input. Status: IN DEVELOPMENT.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
