RL-10B-2
model of rocket engine
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RL-10B-2
Summary
RL-10B-2 is an engine model[1].
Key Facts
- RL-10B-2's image is recorded as Delta IV rocket second stage.jpg[2].
- RL-10B-2's instance of is recorded as engine model[3].
- RL-10B-2's manufacturer is recorded as Pratt & Whitney[4].
- RL-10B-2's subclass of is recorded as RL-10[5].
- RL-10B-2's country of origin is recorded as United States[6].
- RL-10B-2's first flight is recorded as +1998-00-00T00:00:00Z[7].
- RL-10B-2's source of energy is recorded as liquid oxygen[8].
- RL-10B-2's source of energy is recorded as liquid hydrogen[9].
- RL-10B-2's used by is recorded as Delta Cryogenic Second Stage[10].
- RL-10B-2's used by is recorded as Interim Cryogenic Propulsion Stage[11].
- RL-10B-2's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+4.15'}[12].
- RL-10B-2's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+301'}[13].
- RL-10B-2's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+110'}[14].
- RL-10B-2's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.146'}[15].
- RL-10B-2's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+465.5'}[16].
Body
Physical Characteristics
RL-10B-2's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+4.15'}[12].
Designation and Status
RL-10B-2's instance of is recorded as engine model[3].