National Aeronautics and Space Administration

Titan II GLV

GLV

Titan II GLV
Retired

Overview

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The Titan II GLV (Gemini Launch Vehicle) or Gemini-Titan II was an American expendable launch system derived from the Titan II missile, which was used to launch twelve Gemini missions for NASA between 1964 and 1966. Two unmanned launches followed by ten manned ones were conducted from Launch Complex 19 at the Cape Canaveral Air Force Station, starting with Gemini 1 on April 8, 1964.

Manufacturer

National Aeronautics and Space Administration

Variant

GLV

Alias

N/A

Maiden Flight

April 8, 1964

Technical Specifications

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33.2 m

Length

3.05 m

Diameter

0 t

Launch Mass

1913 kN

Liftoff Thrust

3850 kg

LEO Capacity

GTO Capacity

Launch Record

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12

Total Launches

12

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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