Q1187865

The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar, though the spaceplane was cancelled before it could fly. The majority of the launcher's payloads were DoD satellites, for military communications and early warning, though one flight (ATS-6) was performed by NASA. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB.

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1965 — 1982  Wikimedia, Wikidata
SLV-4; SLV-5; SLV-5C; Titan 3C; Titan-3(23)C
height 42 metre, mass 626190 kilogram, payload mass 13100 kilogram, payload mass 3000 kilogram, 
Titan III, Glenn L. Martin Company, United States, 
United States, Dong Fang Hong 2, Ekran, Titan III, 1965, 1960s, 

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Location: KML, Cluster Map, Maps,

Frameless

TITAN IIIC AND GANTRY ON PAD 40 - 23 May 1965

Titan IIIC launch of multiple satellites on 22 Dec 1965

Initial Defense Communications Satellite Program deployment in orbit

Titan III-C Launch - GPN-2003-00046

Titan IIIC launches with ATS-6 from Launch Complex 40

Type	Subtype	Date	Description	Notes	Source
commons	image		TITAN IIIC AND GANTRY ON PAD 40 - 23 May 1965		Commons
commons	image		Titan IIIC launch of multiple satellites on 22 Dec 1965		Commons
commons	image		Initial Defense Communications Satellite Program deployment in orbit		Commons
commons	image		Titan III-C Launch - GPN-2003-00046		Commons
commons	image		Titan IIIC launches with ATS-6 from Launch Complex 40		Commons