AIS-SWAG1-QUAD
Applied Ion Systems
The AIS-SWAG1-QUAD is a Sublimation Warm Gas Thruster designed for CubeSats, offering 480uN of thrust and a total impulse of 12Ns, enabling significant orbital movement for small satellites.
Typed specifications9 values
Discloses 6 of 10 fields engineers filter by in this category (category median 3).
- Mass
- 860 g product page
- Thrust
- 0.48 mN product page
- Envelope (L×W×H)
- 86x86x54 mm product page
- Specific impulse
- 20 s product page
- Total impulse
- 12 N·s product page
- Propellant
- other adamantane (sublimating solid, warm-gas thruster) · product page
- Power consumption
- 20 W product page
- Lead time
- 8 months product page
- Propellant mass (full load)
- 38 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
- Quad Sublimation Warm Gas Thruster
- Fuel
- Solid Unpressurized Adamantane
- Power
- 20 W
- Thrust
- 480uN
- Operating lifetime
- 7 hours
- Pre-heat time
- 1 hour
- Ramp-up time to max thrust
- 3 hours
- Total impulse
- 12Ns
- ISP
- 20s
- Orbital movement (1kg 1U)
- 17.6 km
- Orbital movement (3kg 3U)
- 5.9 km
- Dimensions
- 86x86x54 mm
- Mass
- 860 g
- Fuel mass
- 38 g
- Inputs
- 12 V, 5 V, GND, x1 Logic Command
- Price
- $12,500.00
- Status
- AVAILABLE
- Lead time
- 8 WEEKS
About
The AIS-SWAG1-QUAD is a Sublimation Warm Gas Thruster, part of Applied Ion Systems’ heritage electric and chemical propulsion solutions for the PocketQube and CubeSat market. This thruster utilizes solid unpressurized adamantane as fuel and provides 480uN of thrust with a power consumption of 20W. It boasts an operating lifetime of 7 hours and a total impulse of 12Ns, with an ISP of 20s. The thruster requires a pre-heat time of 1 hour and a ramp-up time to maximum thrust of 3 hours. It is capable of providing 17.6km of orbital movement for a 1kg 1U satellite and 5.9km for a 3kg 3U satellite. The unit measures 86x86x54mm and has a fuel mass of 38g. It operates with 12V and 5V inputs, GND, and one logic command. This thruster is designed for small satellite platforms, offering a compact and efficient propulsion solution for orbital maneuvers.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.