Q2273645: Difference between revisions
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Q2273645
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{{Page|Aerojet General X-8|Classes|U.S. experimental spin-stabilized rocket for very high altitude research}} | {{Page|Aerojet General X-8|Classes|U.S. experimental spin-stabilized rocket for very high altitude research|Aerojet General RTV-A-1, RTV-A-1, X-8}} | ||
Revision as of 13:27, 17 February 2025
The Aerojet General X-8 was an unguided, spin-stabilized sounding rocket designed to launch a 150 lb (68 kg) payload to 200,000 feet (61.0 km). The X-8 was a version of the prolific Aerobee rocket family.
1949
Wikimedia, Wikidata
Aerojet General RTV-A-1, RTV-A-1, X-8
108 produced,
Aerojet, United States Air Force,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Sweden, Tarshish, Aerobee, Dong Fang Hong 2, Ekran, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
AerojetX8| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | AerojetX8 | Commons | ||
