HyNOx-22 Thruster
ISPTech
11-44 N green bipropellant thruster with vacuum heritage, >4,000 ignitions, up to 280 s Isp.
Technical specifications
- Thrust range
- 11-44 N
- Specific impulse
- Up to 280 s
- Continuous operation
- >15 minutes
- Propellant throughput
- >60 kg
- Power (ignition)
- 8.5 W
- Power (valve hit)
- 17 W
- Power (valve hold)
- 2 W
- Mass
- <690 g (with flow control valves)
- Minimum impulse bit (hot)
- <1 Ns
- Minimum impulse bit (cold)
- <50 mNs
- Ignitions demonstrated
- >4,000
- Mounting interface
- 4x M5 (adjustable)
- Propellant
- N2O + C2H6 (self-pressurizing)
- Status
- Available now, qualified for NewSpace customers
About
The HyNOx-22 is a high-performance green bipropellant thruster with demonstrated vacuum heritage. Using nitrous oxide and ethane as self-pressurizing propellants, it delivers 11-44 N of thrust with a specific impulse of up to 280 seconds. With over 4,000 ignitions demonstrated and more than 60 kg of propellant throughput validated, it is available now and qualified for NewSpace customers. The adjustable M5 mounting interface allows flexible integration into various spacecraft platforms.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
