AIS-SWAG1-PQ Sublimation Warm Gas Thruster
Applied Ion Systems
A PocketQube-class sublimation warm gas thruster using solid unpressurized Adamantane propellant, providing 120uN thrust for up to 7 hours of operation.
Typed specifications9 values
Discloses 6 of 10 fields engineers filter by in this category (category median 3).
- Mass
- 214 g product page
- Thrust
- 0.12 mN product page
- Envelope (L×W×H)
- 42x42x54 mm product page
- Specific impulse
- 20 s product page
- Total impulse
- 3 N·s product page
- Propellant
- other adamantane (sublimating solid, warm-gas thruster) · product page
- Power consumption
- 5 W product page
- Lead time
- 4–6 months product page
- Propellant mass (full load)
- 9.5 g product page
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier18 lines, in the manufacturer's own wording
- Type
- Sublimation Warm Gas Thruster
- Fuel
- Solid Unpressurized Adamantane
- Power
- 5 W
- Thrust
- 120uN
- Operating lifetime
- 7 hours
- Pre-heat time
- 1 hour
- Ramp-up time to max thrust
- 3 hours
- Total impulse
- 3Ns
- ISP
- 20s
- Orbital movement (0.75kg 3P)
- 6 km
- Orbital movement (1kg 1U)
- 4.5 km
- Dimensions
- 42x42x54 mm
- Mass
- 214 g
- Fuel mass
- 9.5 g
- Inputs
- 12 V, 5 V, GND, x1 Logic Command
- Price
- $4500.00
- Status
- AVAILABLE
- Lead time
- 4-6 WEEKS
About
The AIS-SWAG1-PQ is a sublimation warm gas thruster using solid unpressurized Adamantane as propellant. Designed for PocketQube and small CubeSat applications, it provides 120uN of thrust at 5W power. The system uses a sublimation heating approach requiring a 1-hour pre-heat time before reaching operational temperatures, with maximum thrust achieved after approximately 3 hours of warm-up. The thruster provides 3Ns of total impulse from 9.5g of Adamantane fuel, enabling approximately 6km of orbital movement for a 0.75kg 3P PocketQube or 4.5km for a 1kg 1U CubeSat. With an unpressurized solid propellant, the system is inherently safe and avoids the complexity of pressure vessels. Status: AVAILABLE.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.