Q17391: Difference between revisions
From Spacefaring
Q17391
Bot: Automated import of articles |
Bot: Automated import of articles *** existing text overwritten *** |
||
| Line 1: | Line 1: | ||
{{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,
Persia, 1950s, Republic of Haiti, 1959, Ekran, Dong Fang Hong 2, Tarshish, Sikh Confederacy, Reman, Ashkenaz, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, France, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent,
-
Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|