R-4D-15 HiPAT
From Spacefaring
model of hypergolic rocket engine
Wikidata
Aerojet R-4D-11 HiPAT; HiPAT; Marquardt R-4D-15 HiPAT; R4D-15 HiPAT
specific impulse by weight 322.2 second, length 70.57 centimetre, length 62.79 centimetre, diameter 36.2 centimetre, diameter 32.51 centimetre, maximum thrust 445 newton, mass 5.2 kilogram, mass 5.44 kilogram,
Aerojet Rocketdyne, United States,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, R-4D, Republic of Haiti,
-
Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|