RL-10A-4-1
model of rocket engine
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RL-10A-4-1
Summary
RL-10A-4-1 is an engine model[1].
Key Facts
- RL-10A-4-1's instance of is recorded as engine model[2].
- RL-10A-4-1's manufacturer is recorded as Pratt & Whitney[3].
- RL-10A-4-1's subclass of is recorded as RL-10A[4].
- RL-10A-4-1's country of origin is recorded as United States[5].
- RL-10A-4-1's first flight is recorded as +2000-00-00T00:00:00Z[6].
- RL-10A-4-1's source of energy is recorded as liquid oxygen[7].
- RL-10A-4-1's source of energy is recorded as liquid hydrogen[8].
- RL-10A-4-1's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+167'}[9].
- RL-10A-4-1's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+99.10'}[10].
- RL-10A-4-1's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.53'}[11].
- RL-10A-4-1's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+451'}[12].
Body
Designation and Status
RL-10A-4-1's instance of is recorded as engine model[2].