RL-10A-5
model of rocket engine
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RL-10A-5
Summary
RL-10A-5 is an engine model[1].
Key Facts
- RL-10A-5's instance of is recorded as engine model[2].
- RL-10A-5's manufacturer is recorded as Pratt & Whitney[3].
- RL-10A-5's subclass of is recorded as RL-10A[4].
- RL-10A-5's country of origin is recorded as United States[5].
- RL-10A-5's first flight is recorded as +1993-00-00T00:00:00Z[6].
- RL-10A-5's source of energy is recorded as liquid oxygen[7].
- RL-10A-5's source of energy is recorded as liquid hydrogen[8].
- RL-10A-5's used by is recorded as McDonnell Douglas DC-X[9].
- RL-10A-5's height is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.07'}[10].
- RL-10A-5's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+143'}[11].
- RL-10A-5's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+64.70'}[12].
- RL-10A-5's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.02'}[13].
- RL-10A-5's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+316'}[14].
Body
Designation and Status
RL-10A-5's instance of is recorded as engine model[2].