AIS-SWAG2-X1 Sublimation Warm Gas Thruster
Applied Ion Systems
A next-generation single-nozzle sublimation warm gas thruster using solid unpressurized Adamantane, providing an estimated 147uN thrust in a 92x92x67mm form factor. In development.
Technical specifications
- Type
- Sublimation Warm Gas Thruster
- Fuel
- Solid Unpressurized Adamantane
- Power
- TBD
- Thrust
- 147uN
- 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-X1 is the next-generation single-nozzle sublimation warm gas thruster at AIS, using solid unpressurized Adamantane as propellant. Housed in a 92x92x67mm form factor, the SWAG2-X1 provides an estimated 147uN of thrust. 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.
