Q17391: Difference between revisions
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Q17391
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{{Page|Antarès|Classes|French experimental sub-orbital rocket designed by ONERA for reentry studies}} | {{Page|Antarès|Classes|French experimental sub-orbital rocket designed by ONERA for reentry studies|OPd-56-39-22D}} | ||
Latest revision as of 13:20, 17 February 2025
The Antarès (OPd-56-39-22D) was a French multistage rocket designed by ONERA for reentry studies. In the late 1950s, the study of missile warhead reentry necessitated the development of a more robust rocket than the existing OR, VD and OPd series. The Antarès rocket, designated OPd-56-39-22D during its developmental phase, was designed to facilitate the study of kinetic heating on objects flying at speeds up to Mach 7.
1959 — 1961
Wikimedia, Wikidata
OPd-56-39-22D
mass 1785 kilogram, length 12.2 metre,
France,
Reman, 1950s, Republic of Haiti, 1959, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Sikh Confederacy, Ashkenaz, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, France, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent,
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Location: KML, Cluster Map, Maps,
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