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HTR
Nammo LOx/Solid hybrid rocket engine.
Thrust
: 30.00 kN (6,744 lbf).
Burn time
: 20 s.
Subtopics
Hybrid Test Rocket
American sounding rocket. Single stage vehicle.
Hybrid Test Rocket-1
LOx/Solid propellant rocket stage. Thrust 30.00 kN.
Family
:
Hybrid
.
Country
:
USA
.
Propellants
:
Lox/Solid
.
Stages
:
Hybrid Test Rocket-1
.
Agency
:
Nammo
.
2007 May 3 -
. 10:50 GMT - .
Launch Site
:
Andoya
.
LV Family
:
HTR
.
Launch Vehicle
:
Hybrid Test Rocket
.
HTR Technology test
- .
Nation
:
USA
.
Agency
:
ARR
,
Nammo
.
Apogee
: 30 km (18 mi).
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