2 stage launch vehicle developed by ABL Space Systems using their E2 RP-1/LOX rocket engine. Nine engines are used in the first stage and one in the second stage. The RS1 is designed to be deployed and launched from any suitably flat site using a containerized launch system transported by trucks.
Specifications
- Thrust
- 485 kN
- Height
- 26.8 m
- Diameter
- 1.83 m
- Launch mass
- —
- Stages
- 2
- Launch cost
- $12M
- LEO capacity
- 1,350 kg
- GTO capacity
- 400 kg
- GEO capacity
- —
- SSO capacity
- 1,000 kg
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
1
Launches with a definitive outcome
Success rate
0%
0 of 1
Current success streak
0
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- RS1 | Maiden Flight — Failure