AJ10-118K

From Spacefaring

(Redirected from AJ10-118K)
Q134974446




model of hypergolic rocket engine

1982 — 2018  Wikimedia, Wikidata
AJ-10-118K; Aerojet AJ10-118K; Aerojet Rocketdyne AJ10-118K
specific impulse by weight 320.5 second, diameter 1.53 metre, length 2.68 metre, mass 275 kilogram, maximum thrust 43.38 kilonewton, 
liquid propellant rocket engine, Aerojet Rocketdyne, Aerojet, United States, 
Reman, 1980s, liquid propellant rocket engine, Republic of Haiti, 1982, Ekran, Dong Fang Hong 2, Tarshish, Sikh Confederacy, United States, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz, 

    ​


Location: KML, Cluster Map, Maps,


    Rocket0728 02Rocket0728 02
    Rocket0728 01Rocket0728 01
    Rocket0728 03Rocket0728 03
    Rocket0728 09Rocket0728 09
    Rocket0728 10Rocket0728 10
    Rocket0728 04Rocket0728 04
    Rocket0728 11Rocket0728 11
    Rocket0728 05Rocket0728 05
    Rocket0728 12Rocket0728 12
    Rocket0728 06Rocket0728 06
      TypeSubtypeDateDescriptionNotesSource
      commonsimageRocket0728 02 Commons
      commonsimageRocket0728 01 Commons
      commonsimageRocket0728 03 Commons
      commonsimageRocket0728 09 Commons
      commonsimageRocket0728 10 Commons
      commonsimageRocket0728 04 Commons
      commonsimageRocket0728 11 Commons
      commonsimageRocket0728 05 Commons
      commonsimageRocket0728 12 Commons
      commonsimageRocket0728 06 Commons
      Retrieved from "https://spacefaring.info/index.php?title=Q134974446&oldid=11692"