AIS-SWAG1-DUO Sublimation Warm Gas Thruster
Applied Ion Systems
A dual-nozzle sublimation warm gas thruster using solid unpressurized Adamantane propellant, providing 240uN thrust from a 10W system for 1U to 3U CubeSats.
Technical specifications
- Type
- Sublimation Warm Gas Thruster
- Fuel
- Solid Unpressurized Adamantane
- Power
- 10W
- Thrust
- 240uN
- Operating Lifetime
- 7 hours
- Pre-Heat Time
- 1 hour
- Ramp-Up Time to Max Thrust
- 3 hours
- Total Impulse
- 6Ns
- ISP
- 20s
- Orbital Movement (1kg 1U)
- 8.8km
- Orbital Movement (3kg 3U)
- 2.9km
- Size
- 86x42x54mm
- Mass
- 430g
- Fuel Mass
- 19g
- Inputs
- 12V, 5V, GND, x1 Logic Command
- Status
- AVAILABLE
- Lead Time
- 4-6 WEEKS
About
The AIS-SWAG1-DUO is a dual-module sublimation warm gas thruster using solid unpressurized Adamantane as propellant. Operating at 10W with dual thruster outputs, it provides 240uN of thrust for up to 7 hours of operation. The system enables approximately 8.8km of orbital movement for a 1kg 1U CubeSat or 2.9km for a 3kg 3U CubeSat. Featuring the same pre-heat and ramp-up characteristics as the SWAG1-PQ, the DUO doubles the propellant load (19g) and total impulse (6Ns) compared to the single unit. Inputs are 12V, 5V, GND, and a single logic command. Status: AVAILABLE.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
