Titan II GLV Vehicle Overview

A complete overview of the Titan II GLV launch vehicle, including launch stats, vehicle info and launch locations.

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Titan II GLV rocket

Basic Info

Name

Titan II GLV

Family

Titan

Manufacturer

First Launch

8 Apr 1964

Successful Launches

12

Failed Launches

0

Rocket Info

Status

Inactive

Stages

2

Length

33.2 m

Diameter

3.05 m

Launch Mass

154 tons

Thrust

1,913 kN

Reusability

Not Reusable

Payload Info

LEO Capacity

3,850 kg

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.

Launch Sites used by Titan II GLV

Cape Canaveral Space Force Station

Cape Canaveral Space Force Station launch site

Historic U.S. military rocket launch site, pivotal in space exploration and national security.

📍 FL, United States
🚀 971 Launches

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