Padside

Lambda 4S

Institute of Space and Astronautical Science · Retired

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The Lambda was an experimental Japanese expendable carrier rocket

Specifications

Thrust
Height
16.5 m
Diameter
0.74 m
Launch mass
9 t
Stages
4
Launch cost
LEO capacity
26 kg
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Vehicle specifications from Launch Library; blanks are unpublished figures.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
20%
1 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