HARDWARE / PRODUCTUpdated 24 Jul 2026

HyNOx 4U CubeSat Propulsion Module

ISPTech
HyNOx 4U CubeSat Propulsion Module

The HyNOx 4U CubeSat Propulsion Module is an integrated propulsion system for CubeSats, featuring a HyNOx-1 thruster and cold/warm gas thrusters, designed for significant deltaV and attitude control.

Key figurescomparable across the catalogue

Mass
2.5 kg
Power
8.5 W
Thrust
2 N
Specific impulse
260 s
Lead time
6 months

Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.

As published by the supplier

Included hardware
1x HyNOx-1 (0.5-2 N, Isp > 260 s)
Included hardware (2)
4x Cold / Warm Gas Thrusters
Status
Available now
Capabiltites
> 4,000 Ns impulse (for standard length)
Capabiltites (2)
0.5-2 N thrust for rapid orbit changes
Capabiltites (3)
Roll, pitch and yaw control
Impulse class
CubeSat Propulsion Systems up to 4,300 Ns
Impulse class (2)
Customized Propulsion Systems starting from 4,300 Ns
Dimensions
4U (209.3×209.3×110.0 mm³)
Dimensions (2)
Z-length adjustable.
Lead time
6 months
Electronics
20-33 VDC Supply Voltage
Electronics (2)
Communication via RS-485 bus (other options possible)
Qualification
According to SpaceX Falcon 9 Payload User Guide (for rideshare missions)

About

The HyNOx 4U CubeSat Propulsion Module is a complete propulsion system offered by ISPTech, specifically designed for 4U CubeSats. It integrates one HyNOx-1 thruster, capable of 0.5-2 N thrust and an Isp of over 260 s, along with four cold/warm gas thrusters for precise attitude control. This module enables significant deltaV for rapid orbit changes and provides roll, pitch, and yaw control. It offers an impulse capability of over 4,000 Ns for the standard length configuration, with customized systems starting from 4,300 Ns. The module has dimensions of 209.3×209.3×110.0 mm³ and features an adjustable Z-length. It operates with a 20-33 VDC supply voltage and communicates via an RS-485 bus, with other communication options available. The system is qualified according to the SpaceX Falcon 9 Payload User Guide for rideshare missions, ensuring its suitability for space deployment. It is available now with a lead time of 6 months. ISPTech also offers a broader range of HyNOx Propulsion Systems, including various HyNOx thrusters (HyNOx-1, HyNOx-5, HyNOx-22, HyNOx-200) and Cold Gas Propulsion Systems, all designed for different spacecraft and mission requirements.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: www.isptech.space ↗

The rest of the range from ISPTech

All 2 products →

Chemical Propulsion 1

Cold Gas Systems 1