Orbital launch vehicle
SL1
3-stage orbital launch vehicle developed by German private company HyImpulse, with capability of up to 600 kg to Low Earth Orbit. All 3 stages are powered by hybrid rocket motors using paraffin and liquid oxygen as fuel.
Flights flown01 scheduled
Payload to LEO600kg
SL1 is built by HyImpulse of Germany. Company background, funding, contracts and news for this operator are tracked on Space Index.
Payload
| Low Earth orbit | 600kg |
|---|
Vehicle
| Stages | 3 |
|---|---|
| Length | 33m |
| Diameter | 2.2m |
| Reusable | No |
Orbits delivered
Low Earth Orbit1
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| TBD | SL1 | Demo Flight | Unknown Pad | Low Earth Orbit | Scheduled |
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.
Further reading: Wikipedia · Operator page
Fewer than three recorded flights, so this page is marked noindex. It is here for completeness, not for search.