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((Short description|Expendable launch system))
((redirect|Gemini-Titan II (rocket)|the space mission|Gemini-Titan 2))
((Use mdy dates|date=February 2015))
((More citations needed|date=September 2020))
((Infobox rocket
|name = Titan II GLV
|image =Gemini-Titan_11_Launch_-_GPN-2000-001020.jpg
|caption = Launch of [[Gemini 11]] on a Titan II GLV from LC-19
|function = [[Human-rated]] [[launch vehicle]] for [[Project Gemini|Gemini]] spacecraft
|manufacturer = [[Glenn L. Martin Company|Martin]]
|country-origin = United States
|height = ((convert|109|ft|abbr=on))<ref>((Citation
  | first = Kenneth | last = Gatland
  | title = Manned Spacecraft
  | place = New York
  | publisher = MacMillan
  | edition = 2nd revision
  | year = 1976
  | page = 37
  | isbn = 0-02-542820-9
  ))
</ref>
|diameter = ((convert|10|ft|abbr=on))
|mass = ((convert|340000|lb|t|abbr=on))
|stages = 2
|capacities =
  ((Infobox Rocket/Payload
  |location =  [[Low Earth orbit|LEO]]((no orbit for payload inline|date=September 2020))
  |kilos    =  ((convert|7900|lb|t|abbr=on))
  ))
|family = [[Titan (rocket family)|Titan]]
|status = Retired
|sites = [[Cape Canaveral Air Force Station|Cape Canaveral]] [[Cape Canaveral Air Force Station Launch Complex 19|LC-19]]
|first= April 8, 1964
|last= November 11, 1966
|launches =12
|success =12
|payloads = [[Project Gemini|Gemini]]
|stagedata =
  ((Infobox Rocket/Stage
  |type       = stage
  |stageno    = First
  |engines    = 1 [[LR87]]-AJ-7
  |thrust     = ((convert|430000|lbf|kN|abbr=on))
  |SI         = 258 [[second|s]]
  |burntime   = 156 seconds
  |fuel       = [[Aerozine 50]] / [[dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]
  ))
  ((Infobox Rocket/Stage
  |type       = stage
  |stageno    = Second
  |engines    = 1 [[LR91]]-AJ-7
  |thrust     = ((convert|100000|lbf|kN|abbr=on))
  |SI         = 316 s
  |burntime   = 180 seconds
  |fuel       = [[Aerozine 50]] / [[dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]
  ))
))

The '''Titan II GLV''' (Gemini Launch Vehicle) or '''Gemini-Titan II''' was an American [[expendable launch system]] derived from the [[LGM-25C Titan II|Titan II missile]], which was used to launch twelve [[Project Gemini|Gemini]] missions for [[NASA]] between 1964 and 1966. Two uncrewed launches followed by ten crewed ones were conducted from [[Cape Canaveral Air Force Station Launch Complex 19|Launch Complex 19]] at the [[Cape Canaveral Air Force Station]], starting with [[Gemini 1]] on April 8, 1964.

The Titan II was a two-stage [[liquid-fuel rocket]], using a [[hypergolic propellant]] combination of [[Aerozine 50]] fuel and [[nitrogen tetroxide]] oxidizer. The first stage was powered by an [[LR87]] engine (with two combustion chambers and nozzles, fed by separate sets of turbomachinery),<ref name="Sutton">((Cite book |last=Sutton |first=George P. |url=https://www.worldcat.org/oclc/63680957 |title=History of liquid propellant rocket engines |date=2006 |publisher=American Institute of Aeronautics and Astronautics |isbn=1-56347-649-5 |location=Reston, Va. |pages=381,384 |oclc=63680957))</ref><ref name="USAFMFACT">((Cite web |title=Aerojet-General LR87 Liquid Rocket |url=http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id%3D888 |url-status=dead |archive-url=https://web.archive.org/web/20101225182027/http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=888 |archive-date=2010-12-25 |access-date=2010-12-25 |website=National Museum of the US Air Force))</ref> and the second stage was propelled by an [[LR-91]] engine.

==Modifications from the Titan II missile==
[[File:Titan II GLV first stage assembly.jpg|thumb|Titan II GLV first stage component assembly scheme.]]
[[File:Titan II GLV second stage assembly.jpg|thumb|Titan II GLV second stage component assembly scheme.]]
[[File:Titan with Gemini Capsule - GPN-2000-001892.jpg|thumb|Titan with Gemini capsule in the Transonic Dynamics Tunnel (1964).]]
In addition to greater payload capability, the Titan II promised greater reliability than the [[Atlas LV-3B]], which had been selected for [[Project Mercury]], because Titan's [[hypergolic propellant|hypergolic]]-fueled engines contained far fewer components.((citation_needed|date=July 2019))

Several modifications were made to the Titan missile to [[human-rating certification|human-rate]] it for Project Gemini:<ref>Simplicity, Duplication Will Give Titan 2 Manned Flight Capability, Aviation Week & Space Technology, September 3, 1962 pages 38-45</ref>

* A "Gemini Malfunction Detection System" was installed to inform the crew of the rocket's status, and improve response in an emergency.
* Redundant systems were installed to reduce the chances of launch failures.
* The inertial guidance system was replaced by a lighter-weight ground-radio guidance system
* The avionics truss in the second stage was modified slightly
* To help guard against the possibility of a guidance malfunction causing the engine nozzles to gimbal hard right or left, an extra backup guidance system was added.
* The second stage propellant tanks were lengthened for longer burn time and unnecessary [[vernier thruster|vernier engines]] and [[retrorocket]]s were removed. Because the second stage engine had had issues with combustion instability, it was equipped with baffled injectors.
* The first stage was loaded with ((convert|13,000|lb|t)) more propellant than the Titan ICBM although the storage tank size remained unchanged.
* Modifications were made to the tracking, electrical and hydraulics systems in the interest of improved reliability.
* The propellants were chilled to slightly improve vehicle performance. This allowed for more mass to be accommodated.
* First stage engine thrust was reduced slightly to cut down on vibration and G loads.
* First stage engine burn would go until propellant depletion unlike Titan ICBMs which were designed to cut off when propellant flow/pressure and engine thrust started dropping as the tanks emptied. This was to prevent the possibility of a malfunctioning pressure sensor triggering an abort condition. Also, running until depletion would slightly boost the Titan's capacity for payload.

Modifications were overseen by the [[Air Force Systems Command]]. The [[Aerojet]] company, the manufacturer of the Titan's engines, had released a revised model during mid-1963 due to deficiencies in the original design, and also to attempt to improve manufacturing procedures.((citation_needed|date=July 2019))

Film footage of [[Gemini 10]]'s launch revealed that the first stage oxidizer tank ruptured shortly after staging and released a cloud of [[dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]. As first stage telemetry had been terminated at staging, there was no data other than photographic/visual evidence to go by, however the conclusion was that either loose debris struck the oxidizer tank dome or else exhaust from the second stage engine had burned through it.((citation_needed|date=July 2019))

[[Gemini 12]]'s launch vehicle also experienced a tank rupture after staging and film review of Titan II ICBM launches found several occurrences of this phenomenon. Since this did not appear to pose any safety risks to the astronauts, NASA decided that it was not a concern.((citation_needed|date=July 2019))

During Titan II ICBM development, it had been found that the first stage turbopump gearbox was prone to total failure caused by resonant vibration in the idler gear. This problem had not occurred on actual launches, but only static firing tests. This was considered to be a critical item to fix. Aerojet developed a totally redesigned gearbox, and all of Gemini launch vehicles except for the uncrewed [[Gemini 1]] used it.((citation_needed|date=July 2019))

There was also a potentially serious problem with the turbopump bearings which led to more design changes, however the odds of failing on a Gemini launch were slim to nil since GLV boosters used specially selected and tested bearings, in addition the turbopumps would be "hot fired" as part of prelaunch checks((citation_needed|date=July 2019))

Combustion instability in the second stage engine was also a concern although that too had only been witnessed in static firing runs. A new injector with improved baffling was developed for the engine and flight-tested on a [[Titan IIIC]] launch; all GLVs from [[Gemini 8]] onwards incorporated it.((citation_needed|date=July 2019))

After a Titan II propellant feed line was found to have some damage  during factory inspections, NASA put out the requirement that all GLV propellant lines had to be [[X-ray]]ed in order to prevent a potentially disastrous fuel leak during launch. X-ray tests later found several more damaged propellant lines, most likely due to careless handling.((citation_needed|date=July 2019))

The most significant issue in man-rating the Titan II was resolving problems with resonant vibration known as "pogo" (since the action was said to resemble that of a [[pogo stick]]) that could produce g-forces sufficient to incapacitate astronauts,((citation needed|date=September 2016)) but the Air Force were not interested in helping NASA with a problem that did not affect the ICBM program and could potentially delay it, or require major modifications to the design. However, Martin-Marietta argued that the pogo problem could be fixed fairly easily, and also the Air Force began to develop more of an interest in man-rating the Titan II due to the proposed [[Manned Orbiting Laboratory]] program. The primary changes made to resolve pogo were adding oxidizer [[standpipe (plumbing)|standpipe]]s, increasing the pressure in the propellant tanks, and adding a mechanical accumulator to the fuel suction side.<ref>Hacker and Grimwood, p. 105</ref>

Another nuisance problem that occurred during the Gemini program was code-named "Green Man" and involved momentary pitch oscillations of the Titan second stage following engine cutoff. This phenomenon had happened on both Gemini and uncrewed Titan II/III flights and had resulted in the failure of the ablative skirt on the second stage at least twice (those instances were dubbed "Brown Man"). Investigation following skirt failure on a Titan IIIC launch concluded that pressure buildup in the ablative skirt caused the pitch oscillations, but NASA decided that there was probably little chance of loose debris from the skirt contacting the Gemini spacecraft, so no corrective action had to be taken and in any case, the Titan IIIC incident was found to be the result of poor quality control which would not affect the more strictly supervised Gemini program.((citation_needed|date=July 2019))

The assembly of these rockets was done at Martin-Marietta's plant in [[Baltimore, Maryland]], so not to interfere with missile work at the one in [[Denver, Colorado]], although this also saved the former plant from a planned shutdown. As with the Mercury-Atlas launch vehicles, a high degree of workmanship was stressed as well as more thorough testing of components and improved handling procedures compared with Titans designed for uncrewed flights. <ref>((cite web|url=https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19780012208_1978012208.pdf |title=New Image - ONLY - Scan to PDF |access-date=2018-10-13))</ref>
((Clear))

==Flights==
[[File:Gemini Profiles.jpg|thumb|right|Titan II GLV launches|400px]]

The Titan II had a much higher thrust-to-weight ratio than the [[Saturn V]]. Astronauts experienced almost 6G before the second stage stopped firing at ((convert|100|mi)) altitude. [[Richard F. Gordon Jr.]] compared the Titan II to "a young fighter pilot's ride. It's faster than the Saturn's old man's ride." [[Frank Borman]] said that simulations did not prepare him for the "almost deafening" noise, which he compared to a jet's afterburner or large train. [[Walter Schirra]] and [[Gordon Cooper]] reported that the ride was smoother than on the Atlas, however.<ref name="agle199809a">((Cite magazine |last=Agle |first=D. C. |date=September 1998 |title=Riding the Titan II |url=https://www.airspacemag.com/flight-today/riding-the-titan-ii-223545/ |magazine=Air & Space |language=en))</ref>

((Clear))
{| class="wikitable"
|-
! Mission
! [[Launch vehicle|LV]]&nbsp;serial&nbsp;No
! Launch date
! Crew
|-
| [[Gemini 1|GT-1]]
| GLV-1 12556
| April 8, 1964
| Uncrewed orbital test flight
|-
| [[Gemini 2|GT-2]]
| GLV-2 12557
| January 19, 1965
| Uncrewed [[sub-orbital spaceflight|suborbital]] test of Gemini heat shield
|-
| [[Gemini 3|GT-3]]
| GLV-3 12558
| March 23, 1965
| [[Gus Grissom]] and [[John Young (astronaut)|John Young]]
|-
| [[Gemini 4|GT-IV]]
| GLV-4 12559
| June 3, 1965
| [[James McDivitt]] and [[Ed White (astronaut)|Ed White]]
|-
| [[Gemini 5|GT-V]]
| GLV-5 12560
| August 21, 1965
| [[Gordon Cooper]] and [[Pete Conrad|Charles P. Conrad]]
|-
| [[Gemini 7|GT-VII]]
| GLV-7 12562 
| December 4, 1965
| [[Frank Borman]] and [[Jim Lovell]]
|-
| [[Gemini 6A|GT-VI A]]
| GLV-6 12561
| December 15, 1965
| [[Wally Schirra]] and [[Thomas P. Stafford]]
|-
| [[Gemini 8|GT-VIII]]
| GLV-8 12563
| March 16, 1966
| [[Neil Armstrong]] and [[David Scott]]
|-
| [[Gemini 9A|GT-IX A]]
| GLV-9 12564
| June 3, 1966
| [[Thomas P. Stafford]] and [[Eugene Cernan]]
|-
| [[Gemini 10|GT-X]]
| GLV-10 12565
| July 18, 1966
| [[John Young (astronaut)|John Young]] and [[Michael Collins (astronaut)|Michael Collins]]
|-
| [[Gemini 11|GT-XI]]
| GLV-11 12566
| September 12, 1966
| [[Pete Conrad|Charles P. Conrad]] and [[Richard F. Gordon Jr.|Richard F. Gordon]]
|-
| [[Gemini 12|GT-XII]]
| GLV-12 12567
| November 11, 1966
| [[Jim Lovell]] and [[Buzz Aldrin|Edwin "Buzz" Aldrin]]
|}

== Displays ==
Two retired [[LGM-25C Titan II|Titan II missiles]] are on display repainted as Gemini Launch Vehicles, along with a few replicas.

* A retired Titan II missile, repainted as ''GLV-3 12558'' (Gemini 3), is on display at [[Rocket garden|KSC Rocket Garden]] since 2010.<ref>((Cite web |author1=Robert Z. Pearlman |date=2010-09-24 |title=Gemini-Titan Rocket Rises Again at Kennedy Space Center |url=https://www.space.com/9194-gemini-titan-rocket-rises-kennedy-space-center.html |access-date=2023-09-20 |website=Space.com |language=en))</ref>
* Another retired Titan II missile, repainted as ''GLV-9 12564'' (Gemini 9A), is on display at the [[Stafford Air & Space Museum]]. <ref>((Cite web |date=2019-03-27 |title=A Field Guide to American Spacecraft |url=http://www.americanspacecraft.com/pages/booster/gt-staff.html |access-date=2023-09-20 |archive-url=https://web.archive.org/web/20190327091710/http://www.americanspacecraft.com/pages/booster/gt-staff.html |archive-date=March 27, 2019 ))</ref>
* A Gemini-Titan II full scale replica was erected for the 1964 [[1964 New York World's Fair|New York World's Fair]]. It remains on display at the [[New York Hall of Science]], [[Flushing Meadows–Corona Park|Corona Park]], NY.<ref>((Cite web |date=2019-03-27 |title=A Field Guide to American Spacecraft |url=http://www.americanspacecraft.com/pages/booster/gt-nyhos.html |access-date=2023-09-20 |archive-url=https://web.archive.org/web/20190327091705/http://www.americanspacecraft.com/pages/booster/gt-nyhos.html |archive-date=March 27, 2019 ))</ref>
* Another full size replica is on display at the [[Cosmosphere|Kansas Cosmosphere and Space Center]].<ref>((Cite web |date=2019-03-27 |title=A Field Guide to American Spacecraft ((!)) KCSC Gemini-Titan |url=http://www.americanspacecraft.com/pages/booster/gt-kcsc.html |access-date=2023-09-20 |archive-url=https://web.archive.org/web/20190327071919/http://www.americanspacecraft.com/pages/booster/gt-kcsc.html |archive-date=March 27, 2019 ))</ref>
* A third replica was displayed at the [[Parque de las Ciencias|Parque de las Ciencias Luis A. Ferré]], [[Bayamón, Puerto Rico|Bayamon]], PR.<ref>((Cite web |date=2019-03-18 |title=A Field Guide to American Spacecraft |url=http://www.americanspacecraft.com/pages/booster/gt-pr.html |access-date=2023-09-20 |archive-url=https://web.archive.org/web/20190318221645/http://www.americanspacecraft.com/pages/booster/gt-pr.html |archive-date=March 18, 2019 ))</ref>
* A mockup, created from two [[HGM-25A Titan I|Titan I]] first stages, was on display at KSC Rocket Garden until 2006.<ref>((Cite web |date=2019-03-27 |title=A Field Guide to American Spacecraft |url=http://americanspacecraft.com/pages/booster/gt-kscvc.html |access-date=2023-09-20 |archive-url=https://web.archive.org/web/20190327165831/http://americanspacecraft.com/pages/booster/gt-kscvc.html |archive-date=March 27, 2019 ))</ref> In 2010 this replica was shipped to [[Johnson Space Center]] in Texas.<ref>((Cite web |title=Rare rocket delivery: Gemini-Titan display arrives in Houston ((!)) collectSPACE |url=http://www.collectspace.com/news/news-063010a.html |access-date=2023-09-20 |website=collectSPACE.com))</ref>
<gallery mode="packed">
File:Gemini-Titan II - Kennedy Space Center - Cape Canaveral, Florida - DSC02349.jpg|Titan II missile, repainted as GLV-3 12558 (Gemini 3), at [[Rocket garden|KSC Rocket Garden]].
File:Stafford Air & Space Museum, Weatherford, OK, US (127).jpg|Titan II missile, repainted as GLV-9 12564 (Gemini 9A), at [[Stafford Air & Space Museum]].
File:NY Hall of science7988.JPG|Gemini-Titan II replica (right) at the [[New York Hall of Science]],
File:Gemini-Titan II Rocket (10531718776).jpg|Gemini-Titan II mockup,  created from two Titan I first stages, at [[Rocket garden|KSC Rocket Garden]].
File:Hutchinson Community College - Kansas Cosmosphere Hutchinson Kansas 9-14-2014.JPG|Gemini-Titan II replica (bottom) at the [[Cosmosphere|Kansas Cosmosphere and Space Center]].
</gallery>

==See also==
*[[SM-65D Atlas]]
*[[Soyuz (rocket)]]
*[[Voskhod (rocket)]]

==References==
((Reflist))

==References==
*((cite web|url=http://space.skyrocket.de/doc_lau_det/titan-2-glv.htm|title=Titan-2-GLV|last=Krebs|first=Gunter|publisher=Gunter's Space Page|access-date=2009-04-29))
*((cite web|url=http://www.astronautix.com/lvs/titan.htm|archive-url=https://web.archive.org/web/20080805095233/http://www.astronautix.com/lvs/titan.htm|url-status=dead|archive-date=August 5, 2008|title=Titan|last=Wade|first=Mark|publisher=Encyclopedia Astronautica|access-date=2009-04-29))

==External links==
((commons category-inline|Titan II Gemini))

((USAF space vehicles))
((Titan rockets))
((Expendable launch systems))
((US launch systems))
((Gemini program))
((NASA space program))

((Use American English|date=January 2014))

((DEFAULTSORT:Titan Ii))
[[Category:Project Gemini]]
[[Category:Titan (rocket family)]]
[[Category:Rockets and missiles]]
[[Category:NASA space launch vehicles]]

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Module:Navbar (view source) (protected)
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Module:Navbar/styles.css (view source) (protected)
Module:Navbox (view source) (template editor protected)
Module:Navbox/configuration (view source) (template editor protected)
Module:Navbox/styles.css (view source) (template editor protected)
Module:Ns has subpages (view source) (protected)
Module:Pagetype (view source) (protected)
Module:Pagetype/config (view source) (protected)
Module:Pagetype/disambiguation (view source) (protected)
Module:Pagetype/setindex (view source) (protected)
Module:Pagetype/softredirect (view source) (protected)
Module:Redirect hatnote (view source) (template editor protected)
Module:SDcat (view source) (protected)
Module:String (view source) (protected)
Module:String2 (view source) (template editor protected)
Module:Unsubst (view source) (protected)
Module:WPMILHIST Infobox style (view source) (template editor protected)
Module:WikidataIB (view source) (template editor protected)
Module:WikidataIB/nolinks (view source) (template editor protected)
Module:WikidataIB/titleformats (view source) (template editor protected)
Module:Wikitext Parsing (view source) (protected)
Module:Yesno (view source) (protected)

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