HARDWARE / PRODUCTAdded 16 Aug 2026

Hybrid Propulsion Systems

HyImpulse Technologies
Hybrid Propulsion Systems

HyImpulse's hybrid motor family powers suborbital and orbital vehicles with lightweight composite casings, thrust vector control, and modular interfaces, providing liquid-like performance with hybrid simplicity.

Key figurescomparable across the catalogue

Thrust
90,000 N

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

Thrust (SL1 orbital launcher)
90 kN
Thrust (SR75 sounding rocket)
75 kN
Thrust (scalable architecture)
10 kN
Propellant
Nitrous oxide hybrid
Casing
Full composite
Features
Throttling, Shutdown & restart, Customizable, Mission-ready & Scalable, ITAR Free, Re-ignitable
Feed System
Pressure or pump-fed

About

Our hybrid motor family powers suborbital and orbital vehicles with lightweight composite casings, thrust vector control, and modular interfaces, providing liquid-like performance with hybrid simplicity. We offer a 90 kN motor that powers the SL1 orbital launcher, successfully hot-fire tested in 2025, and a 75 kN motor that drives the SR75 sounding rocket, validated in flight. Additionally, a 10 kN motor, tested over 100 times, shares the same scalable architecture. These systems build on the flight-proven nitrous oxide hybrid technology used in the HEROS rockets, which flew above 100,000 ft in 2016. In-house turbomachinery and powerpacks further ensure efficient, reliable performance across all missions. Our propulsion systems feature full composite casings, throttling, shutdown & restart capabilities, and are customizable, mission-ready, and scalable. They are ITAR Free, have no restrictions, and are re-ignitable for multiple burns. The feed system can be pressure or pump-fed.

Documentation

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

Source: www.hyimpulse.de ↗

The rest of the range from HyImpulse Technologies

All 5 products →

Launch Vehicles 2

Orbital Transfer Vehicles 1