RD-108-8D77
Soviet liquid rocket engine
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RD-108-8D77
Summary
RD-108-8D77 is an engine model[1].
Key Facts
- RD-108-8D77's instance of is recorded as engine model[2].
- RD-108-8D77's manufacturer is recorded as NPO Energomash[3].
- RD-108-8D77's subclass of is recorded as RD-108[4].
- RD-108-8D77's country of origin is recorded as Soviet Union[5].
- RD-108-8D77's source of energy is recorded as RP-1[6].
- RD-108-8D77's source of energy is recorded as liquid oxygen[7].
- RD-108-8D77's used by is recorded as Sputnik 8A91-1[8].
- RD-108-8D77's height is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.86'}[9].
- RD-108-8D77's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+1250'}[10].
- RD-108-8D77's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+804'}[11].
- RD-108-8D77's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+628'}[12].
- RD-108-8D77's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+0.67'}[13].
- RD-108-8D77's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+315'}[14].
- RD-108-8D77's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+246'}[15].
Body
Designation and Status
RD-108-8D77's instance of is recorded as engine model[2].