The Titan 34D was an American expendable launch vehicle derived from the Titan III and used to launch satellites for military applications. Its first and second stages were stretched and it flew with more powerful UA1206 solid motors. A choice of upper stages was offered, including the Inertial Upper Stage, the Transfer Orbit Stage and the Transtage, and it could lift 14,515 kg to low Earth orbit and 5,000 kg to geostationary transfer orbit. Its first flight was on 30 October 1982, carrying two DSCS defense communications satellites, and fifteen launches in all were made from Launch Complex 40 at Cape Canaveral and Space Launch Complex 4E at Vandenberg, three of which failed. Two of those failures were the loss of a KH-11 satellite on 34D-7 in August 1985 and the explosion of 34D-9 on its pad in April 1986 while carrying the last KH-9 satellite.
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Source Titan 34D (Wikipedia)
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Source Encyclopedia Astronautica: MartinAgency profile of Martin, launch vehicles listQuote, Agency profile of Martin, launch vehicles list
American manufacturer of rockets, spacecraft, and rocket engines. Martin Marietta Astronautics Group (1956), Denver, CO, USA.
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Source Titan 34D (Wikipedia)Lead, country of originQuote, Lead, country of origin
The Titan 34D was a United States expendable launch vehicle
Sources
1. Titan 34D (Wikipedia)
Service history, first flight
The Titan 34D made its maiden flight in the year of 1982 on the 30th of October with two DSCS defense communications satellites
Lead
The Titan 34D was a United States expendable launch vehicle used to launch a number of satellites for military applications.
Service history, stages
Derived from the Titan III, the Titan 34D featured Stage 1 and Stage 2 stretched with more powerful UA1206 solid motors.
Service history, motors
Derived from the Titan III, the Titan 34D featured Stage 1 and Stage 2 stretched with more powerful UA1206 solid motors.
Lead, country of origin
The Titan 34D was a United States expendable launch vehicle
In Group: Orbital Launch Vehicles, Lead, role
The Titan 34D was a United States expendable launch vehicle used to launch a number of satellites for military applications.
Exemplifies: Orbital Spaceflight, Specification
The Titan 34D had a payload capacity of 14,515 kg (32,000 lb) to low Earth orbit, and of 5,000 kg (11,000 lb) to a GTO.
View the Source2. Encyclopedia Astronautica: Titan 34D
Encyclopedia AstronauticaKey factsQuote, Key facts
Status Retired 1988
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