Orbital launch vehicle

RS1

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.

Flights flown1
Success rate0%0/1
Payload to LEO1,350kg
Cost per kg to LEO$8,889$12M per launch
Maiden flight2023-01-10
Peak year20231 flight

RS1 is built by Long Wall of the United States. Company background, funding, contracts and news for this operator are tracked on Space Index. It first flew on 10 January 2023 and last flew on 10 January 2023.

Flight record

1 records
0% success rate0 of 1 flown · 1 failed
First flight2023-01-10
Latest flight2023-01-10
Failures1
Consecutive successes0

Payload

Per mission profile
Low Earth orbit1,350kg
Sun-synchronous orbit1,000kg
Geostationary transfer orbit400kg
Launch cost$12M
Cost per kg to LEO$8,889

Vehicle

1 spec
Stages2
Length26.8m
Diameter1.83m
Liftoff thrust485kN
Maiden flight2023-01-10
ReusableNo

Pads used

1 pad

Orbits delivered

1 orbit
Low Earth Orbit1

Launch history

1 launches
DateMissionPadOrbitOutcome
2023-01-10RS1 | Maiden FlightLaunch Pad 3CLow Earth OrbitFailure

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.