GU-1 Earth Observation CubeSat (6U)
A 6U platform imaging at 3.2 m resolution in a 550 km orbit.
- Launch / deployment platform
- Space
- Launch mass
- 9 kg
- Propulsion
- Electric / none
- Status
- Operational
ÜF-250 Small Satellite Launch Vehicle
A two-stage hybrid–liquid launcher to carry up to 250 kg to low Earth orbit.
The ÜF-250 is a two-stage launcher developed for small satellite constellations and single-satellite missions. It uses a hybrid motor in the first stage and a liquid oxygen–kerosene engine in the second.
Highlights
- Target of carrying 250 kg to a 500 km Sun-synchronous orbit
- Reusable first-stage study
- Mobile launch pad: launch from different sites
Status
The first-stage motor reached 140 kN thrust in static firing tests; the first orbital launch is planned for 2029.
Key features
- 250 kg payload
- Hybrid + liquid
- Mobile pad
Technical specifications
| Payload to LEO | 250 kg |
|---|---|
| First-stage thrust | 140 kN |
| Length | 21 m |
| Liftoff mass | 26 ton |
Documents
Similar items
YM-3 S/X-Band Ground Station Antenna
A fully automatic 3.7 m tracking antenna ground station for low-orbit satellites.
- Launch / deployment platform
- Ground station / padSpace
- Launch mass
- 2,800 kg
- Propulsion
- Electric / none
- Status
- Serial production
ZR-122 Multiple Launch Rocket System
A vehicle-mounted 122 mm rocket artillery system with rapid deployment.
- Launch / deployment platform
- Land
- Range
- 40 km
- Launch mass
- 24,000 kg
- Propulsion
- Solid propellant
- Status
- Serial production