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- Titan_II_GLV diameter "3.048".
- Titan_II_GLV height "33223.2".
- Titan_II_GLV mass "154224.0".
- Titan_II_GLV mass "154224.0".
- Titan_II_GLV abstract "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 8 April 1964.The man-rated Titan II was a liquid-propelled rocket, and consisted of two stages. The first stage was powered by an LR87 engine (although this engine has two combustion chambers and nozzles, it is considered a single unit because both chambers use common turbomachinery), and the second stage was propelled by an LR91 engine.The rockets were purpose-built for the Gemini launches and featured some modifications compared to the Titan missiles. A malfunction detection system was installed to inform the crew of the rocket's status, and improve response in an emergency. Redundant systems were fitted to reduce the chances of launch failures. The Titan II promised greater reliability than the Atlas because of its hypergolically-fueled engines requiring far fewer components, however various dangers remained, such as the possibility of a guidance malfunction causing the engine nozzles to gimbal hard right/left. For this reason, an extra backup guidance system was added. The second stage propellant tanks were lengthened for longer burn time and unnecessary vernier engines and retro-rockets were removed. Because the second stage engine had had issues with combustion instability, it was equipped with baffled injectors. A radio control system replaced the inertial guidance used on the missiles, and modifications were made to the tracking, electrical and hydraulics systems in the interest of improved reliability. Modifications were overseen by the Air Force Systems Command. Aerojet, the manufacturer of the Titan's engines, had released a revised model during mid-1963 due to deficiencies in the original design and also attempting to improve manufacturing procedures.Assembly was done at Martin-Marietta's Baltimore plant so as not to interfere with missile work at the Denver facility, although it also saved the former from a planned shutdown.".
- Titan_II_GLV countryOrigin United_States.
- Titan_II_GLV diameter "3.048".
- Titan_II_GLV finalFlight "1966-11-11".
- Titan_II_GLV height "33.2232".
- Titan_II_GLV launchSite Cape_Canaveral_Air_Force_Station.
- Titan_II_GLV maidenFlight "1964-04-08".
- Titan_II_GLV manufacturer Glenn_L._Martin_Company.
- Titan_II_GLV mass "1.54224E8".
- Titan_II_GLV rocketFunction Launch_vehicle.
- Titan_II_GLV rocketStages "2".
- Titan_II_GLV status "Retired".
- Titan_II_GLV successfulLaunches "12".
- Titan_II_GLV thumbnail Gemini-Titan_11_Launch_-_GPN-2000-001020.jpg?width=300.
- Titan_II_GLV totalLaunches "12".
- Titan_II_GLV wikiPageID "22616314".
- Titan_II_GLV wikiPageRevisionID "588600728".
- Titan_II_GLV caption "Launch of Gemini 11 on a Titan II GLV from LC-19".
- Titan_II_GLV family Titan_(rocket_family).
- Titan_II_GLV first "1964-04-08".
- Titan_II_GLV function "Launch vehicle for Gemini manned spacecraft".
- Titan_II_GLV hasPhotoCollection Titan_II_GLV.
- Titan_II_GLV last "1966-11-11".
- Titan_II_GLV launches "12".
- Titan_II_GLV manufacturer Glenn_L._Martin_Company.
- Titan_II_GLV name "Titan II GLV".
- Titan_II_GLV payloads Project_Gemini.
- Titan_II_GLV sites Cape_Canaveral_Air_Force_Station.
- Titan_II_GLV sites Cape_Canaveral_Air_Force_Station_Launch_Complex_19.
- Titan_II_GLV stages "2".
- Titan_II_GLV status "Retired".
- Titan_II_GLV success "12".
- Titan_II_GLV subject Category:NASA_space_launch_vehicles.
- Titan_II_GLV subject Category:Project_Gemini.
- Titan_II_GLV subject Category:Rockets_and_missiles.
- Titan_II_GLV subject Category:Titan_(rocket_family).
- Titan_II_GLV type Artifact100021939.
- Titan_II_GLV type Conveyance103100490.
- Titan_II_GLV type Craft103125870.
- Titan_II_GLV type Equipment103294048.
- Titan_II_GLV type Instrumentality103575240.
- Titan_II_GLV type NASASpaceVehicles.
- Titan_II_GLV type Object100002684.
- Titan_II_GLV type PhysicalEntity100001930.
- Titan_II_GLV type Rocket104099429.
- Titan_II_GLV type RocketsAndMissiles.
- Titan_II_GLV type Satellite104137444.
- Titan_II_GLV type Spacecraft104264914.
- Titan_II_GLV type Vehicle104524313.
- Titan_II_GLV type Whole100003553.
- Titan_II_GLV type MeanOfTransportation.
- Titan_II_GLV type Rocket.
- Titan_II_GLV type RocketEngine.
- Titan_II_GLV type DesignedArtifact.
- Titan_II_GLV comment "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 8 April 1964.The man-rated Titan II was a liquid-propelled rocket, and consisted of two stages.".
- Titan_II_GLV label "Titan II GLV".
- Titan_II_GLV label "Titan II GLV".
- Titan_II_GLV label "Titan II GLV".
- Titan_II_GLV label "Titan II Gemini LV".
- Titan_II_GLV label "タイタンII GLV".
- Titan_II_GLV sameAs Titan_2_GLV.
- Titan_II_GLV sameAs Titan_II_GLV.
- Titan_II_GLV sameAs タイタンII_GLV.
- Titan_II_GLV sameAs Titan_II_Gemini_LV.
- Titan_II_GLV sameAs Titan_II_GLV.
- Titan_II_GLV sameAs m.05zxhf9.
- Titan_II_GLV sameAs Q1187238.
- Titan_II_GLV sameAs Q1187238.
- Titan_II_GLV sameAs Titan_II_GLV.
- Titan_II_GLV wasDerivedFrom Titan_II_GLV?oldid=588600728.
- Titan_II_GLV depiction Gemini-Titan_11_Launch_-_GPN-2000-001020.jpg.
- Titan_II_GLV isPrimaryTopicOf Titan_II_GLV.
- Titan_II_GLV name "Titan II GLV".