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
maximum thrust 445 newton, specific impulse by weight 322.2 second, mass 5.2 kilogram, mass 5.44 kilogram, diameter 36.2 centimetre, diameter 32.51 centimetre, length 70.57 centimetre, length 62.79 centimetre,
Aerojet Rocketdyne,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran,
-
Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|