HM7A
European rocket engine
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HM7A
Summary
HM7A is an engine model[1].
Key Facts
- HM7A's instance of is recorded as engine model[2].
- HM7A's followed by is recorded as HM7B[3].
- HM7A's manufacturer is recorded as Société européenne de propulsion[4].
- HM7A's subclass of is recorded as cryogenic rocket engine[5].
- HM7A's country of origin is recorded as France[6].
- HM7A's first flight is recorded as +1979-12-24T00:00:00Z[7].
- HM7A's source of energy is recorded as liquid rocket propellant[8].
- HM7A's significant event is recorded as new product development[9].
- HM7A's significant event is recorded as maiden flight[10].
- HM7A's significant event is recorded as last flight[11].
- HM7A's used by is recorded as H8[12].
- HM7A's height is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.71'}[13].
- HM7A's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+149'}[14].
- HM7A's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+61.7'}[15].
- HM7A's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+42.9'}[16].
- HM7A's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+0.93'}[17].
- HM7A's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+443'}[18].
- HM7A's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+308'}[19].
Body
Designation and Status
HM7A's instance of is recorded as engine model[2].