Q24883821: Difference between revisions
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Q24883821
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{{Page|Titan IIIM|Classes|cancelled American expendable launch vehicle}} | {{Page|Titan IIIM|Classes|cancelled American expendable launch vehicle|Titan 3M}} | ||
Latest revision as of 13:29, 17 February 2025
The Titan IIIM was a planned American expendable launch system, intended to launch the Manned Orbiting Laboratory and other payloads. Development was cancelled in 1969. The stretched core stage was used on some versions of the Titan IIIB and the projected UA1207 solid booster rockets were eventually used on the Titan IV.
Wikimedia, Wikidata
Titan 3M
height 39 metre, mass 836560 kilogram, payload mass 17000 kilogram,
Martin Marietta, United States,
United States, Dong Fang Hong 2, Ekran, Titan III,
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Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Dorian 10 | Commons | ||
