HARDWARE / PRODUCTUpdated 22 Jul 2026

SL1 Suborbital Small Launch Vehicle

HyImpulse Technologies
SL1 Suborbital Small Launch Vehicle

HyImpulse Technologies' SL1 — a hybrid-propellant suborbital small launch vehicle for technology demonstration and scientific payloads reaching 150 km apogee.

Key figurescomparable across the catalogue

Payload capacity
600 kg

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

Vehicle type
Suborbital hybrid-propellant launch vehicle
Propellants
N2O oxidizer / HTPB solid fuel (hybrid)
Apogee
~150 km (above Kármán line)
Payload
Technology demonstration and scientific payloads
Predecessor
SR75 sounding rocket (tested at Koonibba, Australia)
Founded
2018, Sindelfingen, Germany (University of Stuttgart spin-off)

About

SL1 is HyImpulse Technologies’ next rocket after the SR75 sounding rocket, designed to carry technology demonstration and scientific payloads to suborbital trajectories reaching approximately 150 km apogee — above the Kármán line and thus providing true space environment exposure. Like all HyImpulse vehicles, SL1 uses hybrid propulsion combining a solid fuel with liquid N2O (nitrous oxide) oxidizer.

The N2O/HTPB (hydroxyl-terminated polybutadiene) hybrid engine combination provides several advantages for SL1: N2O is self-pressurizing at room temperature (no high-pressure oxidizer feed system required), inherently safer than storable liquid bipropellants, and lower cost than LOX cryogenics. The solid fuel grain eliminates complex turbopumps. The result is a vehicle that can be transported and prepared for flight in days rather than weeks.

HyImpulse is headquartered in Sindelfingen, Germany (near Stuttgart), and was founded in 2018 as a spin-off from the Institute of Space Systems at the University of Stuttgart. The company has conducted engine hot-fire tests and launched the SR75 from Southern Launch’s Koonibba Test Range in Australia. SL1 is positioned as a stepping stone toward HyImpulse’s planned orbital small launch vehicle.

Documentation

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

Source: hyimpulse.de ↗

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