American rocket used from 1963 to 1966 for five uncrewed suborbital tests of the Apollo spacecraft launch escape system and of the command module parachute recovery system in abort mode.
Specifications
- Thrust
- —
- Height
- 26.2 m
- Diameter
- 3.9 m
- Launch mass
- —
- Stages
- 1
- Launch cost
- —
- LEO capacity
- —
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
5
Launches with a definitive outcome
Success rate
80%
4 of 5
Current success streak
1
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
- Little Joe II | A-004 — Success
- Little Joe II | A-003 — Failure
- Little Joe II | A-002 — Success
- Little Joe II | A-001 — Success
- Little Joe II | QTV — Success