Included Light, Camera and support object. [citation needed], The first guidance system for the Titan III used the AC Spark Plug company IMU (inertial measurement unit) and an IBM ASC-15 guidance computer from the Titan II. The HGM-25A Titan I, built by the Martin Company, was the first version of the Titan family of rockets. The control panel showing the 3 targets of the Titan II missile. The 54 Titan IIs[21] in Arizona, Arkansas, and Kansas[18] were replaced in the U.S. arsenal by 50 MX "Peacekeeper" solid-fuel rocket missiles in the mid-1980s; the last Titan II silo was deactivated in May 1987. It used an Inertial measurement unit made by AC Spark Plug derived from original designs from the Charles Stark Draper Laboratory at MIT. 2. Descend 55 steps beneath the ground to reach the control center. Titans that carried Solid Rocket Boosters (SRBs) (Titan IIIC, IIID, 34D, and IV) had a second ISDS that consisted of several lanyards attached to the SRBs that would trigger and automatically destroy them if they prematurely separated from the core, said "destruction" consisting mainly of splitting the casings open to release the pressure inside and terminate thrust. The Titan IIIA (an early test variant flown in 1964-65) and IIIB (flown from 1966-87 with an Agena D upper stage in both standard and extended tank variants) had no SRMs. The Titan rocket family was established in October 1955 when the Air Force awarded the Glenn L. Martin Company (later Martin Marietta and now Lockheed Martin) a contract to build an intercontinental ballistic missile (SM-68). Il Titan è una famiglia di razzi vettori statunitensi non riutilizzabili. Titan MPRL Faction NATO LDF CSAT AAF Type Surface-to-Air Missile Launcher Calibre 127 mm Magazine capacity 1 Mass 140 Variants Titan MPRL Compact, Static Titan Launcher (AA) Games Thankfully, they never did. The main reason was to reduce the cost of maintenance by $72 million per year; the conversions were completed in 1981. The Titan I could hold a W38 or W49 warhead with explosive power of 3.75 megatons or 1.44 megatons respectively. Larson, Paul O. On September 19, 1980, a second tragedy struck the 308th Strategic Missile Wing. A Titan IIIC in November 1970 failed to place its missile early warning satellite in the correct orbit due to a Transtage failure and a 1975 launch of a DSCS military comsat left in LEO by another Transtage failure. In September 1980, at Titan II silo 374-7 near Damascus, Arkansas, a technician dropped an 8 lb (3.6 kg) socket that fell 70 ft (21 m), bounced off a thrust mount, and broke the skin of the missile's first stage,[11] over eight hours prior to an eventual explosion. Titan III Rocket Missile 3D Model . RSO T+480 seconds. I Titan più recenti sono chiamati Titan-Centaur perché utilizzano un ultimo stadio Centaur.In passato esisteva anche la versione Titan-Agena, in cui l'ultimo stadio era costituito da un razzo Agena.La maggior parte dei razzi vettore Titan sono derivati dal missile balistico intercontinentale Titan II. Select from premium Titan Missile of the highest quality. Stock Footage ID: D378_159_211. [25][26], The Titan IIIA was a prototype rocket booster and consisted of a standard Titan II rocket with a Transtage upper stage. Unlike decommissioned Thor, Atlas, and Titan II missiles, the Titan I inventory was scrapped and never reused for space launches or RV tests, as all support infrastructure for the missile had been converted to the Titan II/III family by 1965. Pages 61–65. The space launch vehicle versions contributed the majority of the 368 Titan launches, including all the Project Gemini crewed flights of the mid-1960s. "Navigation of the Titan IIIC space launch vehicle using the Carousel VB IMU". The Titan IVB was the last Titan rocket to remain in service, making its penultimate launch from Cape Canaveral on 30 April 2005, followed by its final launch from Vandenberg Air Force Base on 19 October 2005, carrying the USA-186 optical imaging satellite for the National Reconnaissance Office (NRO). ", "Titan warhead is reported lying in Arkansas woods", "Titan II: 54 accidents waiting to happen", "America's last Titan 2 nuclear missile is deactivated", "U.S. weather satellite finally escapes grasp of hard luck", http://www.dtic.mil/dtic/tr/fulltext/u2/a007056.pdf, https://en.wikipedia.org/w/index.php?title=Titan_(rocket_family)&oldid=991137754, Intercontinental ballistic missiles of the United States, Military space program of the United States, Articles with unsourced statements from July 2019, Articles with unsourced statements from January 2018, Creative Commons Attribution-ShareAlike License, Thicker tank walls and ablative skirts to support the added weight of upper stages, Radio ground guidance in place of the inertial guidance on ICBM Titan IIs, Guidance package placed on the upper stages (if present), Removal of retrorockets and other unnecessary ICBM hardware. Site Configuration. Choose a size. By RetroFootage Editorial. Handmade Aviation Tags. On March 25, 1978, a launch of a DSCS satellite ended up in the Atlantic Ocean when the Titan second stage hydraulic pump failed, resulting in engine shutdown approximately 470 seconds after launch. While the Polaris, a solid-fuel missile, was developed at the same time as the Titan missiles for use in submarines, the military was attached to the Titan II for diplomatic reasons. Most of the Titan rockets were the Titan II ICBM and their civilian derivatives for NASA. [citation needed], For orbital launches, there were strong advantages to using higher-performance liquid hydrogen or RP-1 (kerosene) fueled vehicles with a liquid oxygen oxidizer; the high cost of using hydrazine and nitrogen tetroxide, along with the special care that was needed due to their toxicity, were a further consideration. [2] Using radar data, it made course corrections during the burn phase. The fifth Titan IIIC (August 26, 1966) failed shortly after launch when pieces of the payload fairing started breaking off. Le lanceur est dérivé du missile balistique intercontinental SM-68 Titan et est caractérisé par le recours à des ergols hypergoliques stockables. Buy clothing, informative books and scale models of the Titan II Missile. The fuel was Aerozine 50, a 50/50 mix of hydrazine and UDMH, and the oxidizer was nitrogen tetroxide. U.S. Air Force photo. Chicano Federal. An airman dropped a wrench socket and it fell 80 feet and pierced the thin skin of the … The missile guidance computer (MGC) was the IBM ASC-15. USAF Sheppard Technical Training Center. The second core stage, the Titan 3A-2, contained about 55,000 lb (25,000 kg) of propellant and was powered by a single Aerojet LR-91-AJ9, which produced 453.7 kN (102,000 lbf) for 145 seconds.[4]. Lockheed Martin decided to extend its Atlas family of rockets instead of its more expensive Titans, along with participating in joint-ventures to sell launches on the Russian Proton rocket and the new Boeing-built Delta IV class of medium and heavy-lift launch vehicles. Find the perfect Titan Missile stock photos and editorial news pictures from Getty Images. "Navigation of the Titan IIIC space launch vehicle using the Carousel VB IMU." The Aerozine 50 and NTO were stored in structurally independent tanks to minimize the hazard of the two mixing if a leak should have developed in either tank. the memory of this part of Cold War history and educating visitors. The Titan III family consisted of an enhanced Titan II core with or without solid rocket strap-on boosters and an assortment of upper stages. They were all launched from Vandenberg Air Force Base, California, due south over the Pacific into polar orbits. [24], The more-advanced Titan IIIC used Delco's Carousel VB IMU and MAGIC 352 Missile Guidance Computer (MGC). All of the launches were successful. All were launched from th… Jusqu'à 63 missiles ont été déployés sur le territoire des États-Unis contigus entre 1963 et 1987… 73-905. Titan was a family of United States expendable rockets used between 1959 and 2005. Some families include both missiles and carrier rockets; they are listed in both groups. For the Titan III, the ASC-15 drum memory of the computer was lengthened to add 20 more usable tracks, which increased its memory capacity by 35%. At a silo outside Rock, Kansas, an oxidizer transfer line carrying nitrogen tetroxide (NTO) ruptured on August 24, 1978. Stage 0: Empty 33,798 kg/ea; Full 226,233 kg/ea. As the IIIC consisted of mostly proven hardware, launch problems were generally only caused by the upper stages and/or payload. Launch Vehicle: Titan II. Each motor composed of five segments and was 10 ft (3.0 m) in diameter, 85 ft (26 m) long, and weighed nearly 500,000 lb (230,000 kg). To get a sense of how large the Titan was, the currently-deployed Minuteman missile weighs a third as much and its warhead has 1/25 the yield. Des versions de plus en plus puissantes ont été développées pou… The Titan II's hypergolic fuel and oxidizer ignited on contact, but they were highly toxic and corrosive liquids. It was a two-stage rocket operational from early 1962 to mid-1965 whose LR-87 booster engine was powered by RP-1 and liquid oxygen. May 1967. Titan I Intercontinental Ballistic Missile (ICBM) Titan I ICBM on display at the Air Force Space and Missile Museum. The Titan Missile Museum, located in a former missile silo, is dedicated to preserving. Two airmen were performing maintenance at Missile Complex 374-7, located 3 miles north of Damascus, the evening of September 18th. Titan III: Research and Development for Today And Tomorrow, https://en.wikipedia.org/w/index.php?title=Titan_IIIC&oldid=998097466, Creative Commons Attribution-ShareAlike License, Transtage failed in low Earth orbit due to oxidizer tank leak, Transtage failed during 3rd burn due to stuck oxidizer valve; left payloads in. Shop with confidence. "Titan III Inertial Guidance System," in AIAA Second Annual Meeting, San Francisco, 26–29 July 1965, pages 1–11. Available at WikiMedia Commons: TitanII MGC.pdf. Starting in the late 1980s, some of the deactivated Titan IIs were converted into space launch vehicles to be used for launching U.S. Government payloads. [23], The Titan III was a modified Titan II with optional solid rocket boosters. Anyone searching for a truly unique overnight adventure has hit the target with a stay at the Titan II Nuclear Missile Complex. Payload fairing broke up at T+78 seconds. The Titan missile, deployed from 1959 to 1987 was the largest ICBM deployed by the United States and delivered a 9 megaton nuclear bomb. The Titan II Missile sites were located in three places in the U.S. as a deterrent to nuclear war during the cold war period–Arkansas, Kansas and Arizona and they were manned 24/7 for 24 years, from 1963 to 1987. Around 80 seconds, the remainder of the shroud disintegrated, causing loss of launch vehicle control as well as the payload (a group of IDCSP satellites intended to provide radio communication for the US Army in Vietnam). Titan IVs were also launched from the Cape Canaveral Air Force Station in Florida for non-polar orbits. Slightly larger propellant tanks in the second stage for longer burn time; since they expanded into some unused space in the avionics truss, the actual length of the stage remained unchanged. 1920 x 1080 H.264. The ISDS would end up being used a few times over the Titan's career. [6] The liquid fuel missiles were prone to developing leaks of their toxic propellants. Its two Aerojet AJ-10-138 engines were restartable, allowing flexible orbital operations including orbital trimming, geostationary transfer and insertion, and delivery of multiple payloads to different orbits. The solid-fuel boosters that were developed for the Titan IIIC represented a significant engineering advance over previous solid-fueled rockets, due to their large size and thrust, and their advanced thrust-vector control systems. Art Drawings Sketches . Nation: USA. The Titan II used the LR-87-5 engine, a modified version of the LR-87, that used a hypergolic propellant combination of nitrogen tetroxide for its oxidizer and Aerozine 50 (a 50/50 mix of hydrazine and UDMH) instead of the liquid oxygen and RP-1 propellant of the Titan I. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB. Thirty-three Titan-II Research Test (N-type) missiles were built and all but one were launched either at Cape Canaveral Air Force Station, Florida, or Vandenberg Air Force Base, California, in 1962–64. The Titan MPRL Compact (full name: Titan Multi-Purpose Rocket Launcher - Compact) is a 127 mm missile launcher used by several BLUFOR, OPFOR and Independent factions in ArmA 3. Paul O. Larson. Le LGM-25C Titan II est un missile balistique intercontinental conçu et mis au point par la Glenn L. Martin Company pour l'US Air Force. By the time the Titan IV became operational, the requirements of the Department of Defense and the NRO for launching satellites had tapered off due to improvements in the longevity of reconnaissance satellites and the declining demand for reconnaissance that followed the internal disintegration of the Soviet Union. [15][16][17] There was one fatality and 21 were injured,[18] all from the emergency response team from Little Rock AFB. The first Titan II guidance system was built by AC Spark Plug. The first stage was powered by a pair of improved LR-87 rocket engines. This required complex guidance and instrumentation. A number of HGM-25A Titan I and LGM-25C Titan II missiles have been distributed as museum displays across the United States. There were several accidents in Titan II silos resulting in loss of life and/or serious injuries. Clip length: 01:25. [citation needed], The Titan III core was similar to the Titan II, but had a few differences. A subsequent version of the Titan family, the Tit… [1] The Titan III launchers provided assured capability and flexibility for launch of large-class payloads. Titan III/IV SRBs were fixed nozzle and for roll control, a small tank of nitrogen tetroxide was mounted to each motor. First Titan flight test missile delivered - . By entering the Museum facility and/or participating in a Museum activity or event, you consent to and authorize without restriction or compensation the possible use of your image and your accompanying group’s image appearing in photograph, audio, video or other formats which may be included in future media or marketing. Let’s explore this underground retreat in 3, 2, 1: We’re aware that these uncertain times are limiting many aspects of life. [13][19] The explosion blew the 740-ton launch tube cover 200 ft (60 m) into the air and left a crater 250 feet (76 m) in diameter.[20]. As a result of these events and improvements in technology, the unit cost of a Titan IV launch was very high. The second launch in October 1965 failed when the Transtage suffered an oxidizer leak and was unable to put its payload (several small satellites) into the correct orbit. Up to 6,600 lb (3,000 kg) into a geosynchronous transfer orbit when launched from, This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future, * - Japanese projects using US rockets or stages, This page was last edited on 3 January 2021, at 20:19. [28][29], The Titan IV was an extended length Titan III with solid rocket boosters on its sides. Transtage inertial measurement unit failure caused it to be stranded in low Earth orbit. La NASA l'a également utilisé de manière marginale pour lancer tous les vaisseaux du programme Gemini ainsi que quelques sondes spatiales telles que Cassini. The Titan 3 missile merges the technologies of the liquid fuel missiles and the solid fuel missiles. Titan I and Titan II were part of the US Air Force's intercontinental ballistic missile fleet until 1987. The Martin Company was able to improve the design with the Titan II. It was a two-stage rocket operational from early 1962 to mid-1965 whose LR-87 booster engine was powered by RP-1 and liquid oxygen. Release: Editorial. [2] Solid motor jettison occurred at approximately 116 seconds.[3]. Modeled in Blender. Check out our titan missiles selection for the very best in unique or custom, handmade pieces from our shops. This rocket was used almost exclusively to launch US military or Central Intelligence Agency payloads. LV Family: Titan. Additional expenses were generated by the ground operations and facilities for the Titan IV at Vandenberg Air Force Base for launching satellites into polar orbits. Their maximum payload mass was about 7,500 lb (3,000 kg). The upper stage, the Titan Transtage, also burned Aerozine 50 and NTO. This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future, This page was last edited on 28 November 2020, at 13:27. The solid motors were ignited on the ground and were designated "stage 0". Titan missile A-3, now scheduled for the first Titan flight test, was delivered to the Air Force by the Martin Company.. 1959 January 19 - . Ce successeur du missile Titan I d'une portée de 10 000 km est capable de lancer une charge deux fois plus lourde que son prédécesseur et contrairement à ce dernier utilise des ergols dits « stockables ». AIAA Paper No. All Solid Rocket Motor (SRM)-equipped Titans (IIIC, IIID, IIIE, 34D, and IV) launched with only the SRMs firing at liftoff, the core stage not activating until T+105 seconds, shortly before SRM jettison. The HGM-25A Titan I, built by the Martin Company, was the first version of the Titan family of rockets. The U.S. Air Force and the BLM partnered in the conversion of Titan Missile Site 570-3 into a historical interpretive site, this site is one of 18 across our state. All Titan II/III/IV vehicles contained a special range safety system known as the Inadvertent Separation Destruction System (ISDS) that would activate and destroy the first stage if there was a premature second stage separation. Silo-launched Titan approved. Titan Missile Museum, Sahuarita Picture: 3 - Check out Tripadvisor members' 1,050 candid photos and videos. Minuteman missile and Titan II missile blast out of missile silos. The exact reason for the shroud failure was not determined, but the fiberglass payload shrouds used on the Titan III up to this point were replaced with a metal shroud afterwards. The ground guidance for the Titan was the UNIVAC ATHENA computer, designed by Seymour Cray, based in a hardened underground bunker. [citation needed], The Titan IIIE, with a high-specific-impulse Centaur upper stage, was used to launch several scientific spacecraft, including both of NASA's two Voyager space probes to Jupiter, Saturn and beyond, and both of the two Viking missions to place two orbiters around Mars and two instrumented landers on its surface. More Than 4,000 Martin Co. There are six former Titan I missile complexes in Colorado. [5] The Titan II was deployed in a 1×9 configuration. Several Atlas and Titan I rockets exploded and destroyed their silos. Titan I's were configured with three missiles per site, with the first missile taking at least 15 minutes, and the 2nd and 3rd missiles in 7 1/2 minutes to launch. 4. A subsequent version of the Titan family, the Titan II, was similar to the Titan I, but was much more powerful. Commercial uses may be available, contact us. Image show & rendered using Cycle render. 73-905. AIAA Paper No. Employes in the Denver Area Witness the Award Presentation Friday A Titan 3 missile is in the background as the Air Force... Lowry Air Force Base* Titan Missile Base; Fidel Salazar of Phoenix, Ariz., cuts away bolts with a cutting torch. The Godly man. The Titan II used the LR-87-5 engine, a modified version of the LR-87, that used a hypergolic propellant combination of nitrogen tetroxide for its oxidizer and Aerozine 50 (a 50/50 mix of hydrazine and UDMH) instead of the liquid oxygen and RP-1 propellant of the Titan I. In August 1965, 53 construction workers were killed in Arkansas when hydraulic fluid used in the Titan II caught fire from a welder's torch in a missile silo northwest of Searcy. [22] The 54 Titan IIs had been fielded along with a thousand Minuteman missiles from the mid-1960s through the mid-1980s. 1959 - The Titan A-3 missile is launched at Cape Canaveral. For the graphics card by, Stakem, Patrick H. The History of Spacecraft Computers from the V-2 to the Space Station, 2010, PRB Publishing, ASIN B004L626U6. However, it was also used for a purely scientific purpose to launch the NASA–ESA Cassini / Huygens space probe to Saturn in 1997. [12] The puncture occurred about 6:30 p.m.[13] and when a leak was detected shortly after, the silo was flooded with water and civilian authorities were advised to evacuate the area. Prison Art Prison Cell American System Reform Movement Innocent People County Jail. [3] The USGS was already in use on the Titan III space launcher when work began in March 1978 to replace the Titan II guidance system. The 98-foot-long, two-stage missile was fueled by kerosene (RP-1 fuel) and liquid oxygen, and was designed to carry nuclear warheads. The primary intelligence agency that needed the Titan IV's launch capabilities was the National Reconnaissance Office (NRO). [citation needed], The Titan V was a proposed development of the Titan IV, that saw several designs being suggested. The last IIIC was launched in March 1982. Titan I missile. If the call ever came through to launch it would take between 3 and a half and 5 minutes before the missile would launch. Test launch of a Titan II from a silo. The Titan Missile Museum, also known as Air Force Facility Missile Site 8 or as Titan II ICBM Site 571-7, is a former ICBM missile site located at 1580 West Duval Mine Road, Sahuarita, Arizona in the United States. [citation needed]. Liang, A.C. and Kleinbub, D.L. Most of the Titan rockets were the Titan II ICBM and their civilian derivatives for NASA. Designated as LGM-25C, the Titan II was the largest USAF missile at the time and burned Aerozine 50 and nitrogen tetroxide (NTO) rather than RP-1 and LOX. AIAA Guidance and Control Conference, Key Biscayne, FL, 20–22 August 1973. These included:[citation needed], The Titan III family used the same basic LR-87 engines as Titan II (with performance enhancements over the years), however SRB-equipped variants had a heat shield over them as protection from the SRB exhaust and the engines were modified for air-starting. PlaneTags are: Authentic - made from actual retired aircraft fuselage, not merely stamped metal. This preserved Titan II missile site, officially known as complex 571-7, is all that remains of the 54 Titan II missile sites that were on alert across the United States from 1963 to 1987. It was developed on behalf of the United States Air Force as a heavy-lift satellite launcher to be used mainly to launch American military payloads and civilian intelligence agency satellites such as the Vela Hotel nuclear-test-ban monitoring satellites, observation and reconnaissance satellites (for intelligence-gathering), and various series of defense communications satellites. The same first-stage rocket engine was used with some modifications. This was to protect the engines from the heat of the SRB exhaust. [8] A staff sergeant of the maintenance crew was killed while attempting a rescue and a total of twenty were hospitalized.[9]. When spares for this system became hard to obtain, it was replaced by a more modern guidance system, the Delco Electronics Universal Space Guidance System (USGS). It began as a backup ICBM project in case the SM-65 Atlas was delayed. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar, though the spaceplane was cancelled before it could fly. The third launch in December experienced a similar failure. [30] Another used a cryogenic first stage with LOX/LH2 propellants; however the Atlas V EELV was selected for production instead. A.C. Liang and D.L. This combination was used to launch the KH-8 GAMBIT series of intelligence-gathering satellites. The final such vehicle launched a Defense Meteorological Satellite Program (DMSP) weather satellite from Vandenberg Air Force Base, California, on 18 October 2003. Main floor of the Launch Control Center inside a long abandoned Titan Missile Silo near Tucson, Arizona, where crews had the ability to launch a nuclear warhead if the orders came. Find great deals on eBay for titan 2 missile. Another site at Potwin, Kansas leaked NTO oxidizer in April 1980 with no fatalities,[10] and was later closed. The RP-1/LOX combination was replaced by a room-temperature fuel whose oxidizer did not require cryogenic storage. Designated the Titan 3A-1, this stage was powered by a twin nozzle Aerojet LR-87-AJ9 engine [4] that burned about 240,000 lb (110,000 kg) of Aerozine 50 and nitrogen tetroxide (NTO) and produced 1,941.7 kN (436,500 lbf) thrust over 147 seconds. 5. Titan II ICBM (SM-68B) The Titan II ICBM, developed from the Titan I missile, was first flown successfully on 16 March 1962. Titan vehicles were also used to lift US military payloads as well as civilian agency intelligence-gathering satellites and to send highly successful interplanetary scientific probes throughout the Solar System. The Titan rocket family was established in October 1955 when the Air Force awarded the Glenn L. Martin Company (later Martin Marietta and now Lockheed Martin) a contract to build an intercontinental ballistic missile (SM-68). consisted of nine separate launch facilities, each housing a single missile . [citation needed], The Titan IIID was the Vandenberg Air Force Base version of the Titan IIIC, without a Transtage, that was used to place members of the Key Hole series of reconnaissance satellites into polar low Earth orbits. Twelve Titan II GLVs were used to launch two U.S. uncrewed Gemini test launches and ten crewed capsules with two-person crews. Second stage hydraulics pump failure. [citation needed], Most of the decommissioned Titan II ICBMs were refurbished and used for Air Force space launch vehicles, with a perfect launch success record. Each squadron. RSO T+83 seconds. (Photos: Richard Kruse, 2009) Titan II. "Titan III Inertial Guidance System," page 4. 3. The surviving N-10, AF Ser. The diameter of the second stage was increased to match the first stage. Both stages of the Titan I used kerosene (RP-1) and liquid oxygen (LOX) as propellants. The Titan I was deployed in a 3×3 configuration, meaning a squadron of nine mis­siles was divided into three, three-missile launch complexes. It landed harmlessly several hundred feet away. It began as a backup ICBM project in case the SM-65 Atlas was delayed. Transtage 3rd burn failure left satellite in unusable lower than planned orbit. The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. The Range Safety destruct command was sent, but it was unclear if the stage received it or if it had already broken up by that point. "Student Study Guide, Missile Launch/Missile Officer (LGM-25)." The targets of these are unknown. Titan I. [citation needed], The Titan IIIB with its different versions (23B, 24B, 33B, and 34B) had the Titan III core booster with an Agena D upper stage. Both stages of the Titan I used kerosene (RP-1) and liquid oxygen (LOX) as propellants. Up to 28,900 lb (13,100 kg) into a low Earth orbit with 28 degrees inclination. Afterward, purchase souvenirs from the Titan Missile Museum gift shop. One Titan V proposal was for an enlarged Titan IV, capable of lifting up to 90,000 pounds (41,000 kg) of payload.