H-1-3
Gross Mass
: 2,200 kg (4,800 lb).
Empty Mass
: 360 kg (790 lb).
Thrust (vac)
: 77.400 kN (17,400 lbf).
Isp
: 291 sec.
Burn time
: 68 sec.
Propellants
:
Solid
.
Isp(sl)
: 220 sec.
Diameter
: 1.34 m (4.39 ft).
Span
: 1.34 m (4.39 ft).
Length
: 2.34 m (7.67 ft).
Country
:
Japan
.
No Engines
: 1.
Engine
:
H-1-3
.
Cost $
: 10.000 million.
First Flight
: 1986.
Last Flight
: 1992.
No Launched
: 9.
Other designations
: UM-129A.
Used on Launch Vehicles:
H-1
.
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