Launch of a Titan IIIE with Voyager 2
|Function||Expendable launch system|
|Country of origin||USA|
|Height||48 m (157 ft)|
|Diameter||3.05 m (10.0 ft)|
|Mass||632,970 kg (1,395,460 lb)|
|15,400 kg (34,000 lb)|
Heliocentric orbit (TMI)
|3,700 kg (8,200 lb)|
|Launch sites||LC-41, Cape Canaveral|
|First flight||11 February 1974|
|Last flight||5 September 1977|
|Notable payloads||Voyager (1 / 2)
Viking (1 / 2)
|Boosters (Stage 0)|
|Thrust||5,849 kN (1,315,000 lbf)|
|Specific impulse||263 sec|
|Burn time||115 seconds|
|Thrust||2,340 kN (530,000 lbf)|
|Specific impulse||302 sec|
|Burn time||147 seconds|
|Thrust||454 kN (102,000 lbf)|
|Specific impulse||316 sec|
|Burn time||205 seconds|
|Third Stage - Centaur-D|
|Thrust||131 kN (29,000 lbf)|
|Specific impulse||444 sec|
|Burn time||470 seconds|
|Fourth Stage (optional) - Star-37E|
|Thrust||68 kN (15,000 lbf)|
|Specific impulse||284 sec|
|Burn time||42 seconds|
The Titan IIIE or Titan 3E, also known as Titan III-Centaur was an American expendable launch system. Launched seven times between 1974 and 1977, it enabled several high-profile NASA missions, including the Voyager and Viking planetary probes, and the joint West German-US Helios spacecraft. All seven launches were conducted from Launch Complex 41 at Cape Canaveral.
In 1967, NASA began considering the possibility of combining the massive Titan III booster and Centaur high-energy upper stage to create what was at the time the most powerful launch vehicle for planetary exploration. With over three times the payload capacity of the Atlas-Centaur, Titan IIIE would be able to launch ambitious robotic spacecraft missions planned for the 1970s.
NASA's Lewis Research Center (now the Glenn Research Center) was given the task of integrating Titan with Centaur, which required a number of modifications to accommodate the more powerful booster. The most obvious change was enclosing Centaur in a large shroud that protected the stage and the payload during ascent. This enabled the use of improved insulation on Centaur, which increased coast time in orbit from 30 minutes when launched on Atlas to over 5 hours on the Titan IIIE. Since Centaur was wider than the Titan's core stage, a tapering interface was required. This interface had to be insulated to prevent boiloff of Centaur's cryogenic propellants, since Titan used hypergolic propellants stored at ambient temperature, while Atlas used liquid oxygen. The Centaur stage also contained the guidance computer for the entire launch vehicle.
A four-stage configuration, with an additional upper stage, a Star-37E, was also available, and was used for the two Helios launches. Star-37E stages were also used on the two Voyager launches, but were considered to be part of the payload rather than the rocket.
The first Titan IIIE launch occurred on February 11, 1974. Original plans were to fly a boilerplate Viking probe, but NASA decided to add a secondary payload: a test satellite called SPHINX (Space Plasma High Voltage Interaction Experiment) which was intended to test the operation of high voltage power supplies in the vacuum of space. The launch proceeded normally through the Titan booster phase lasting about eight minutes, but after separation the Centaur's engines failed to start. Ground controllers issued a manual start command, which also failed to start the engines. About 12 minutes after liftoff, with no power and the vehicle in freefall, the flight was terminated by a range safety destruct command sent from a radar station in Antigua.
The failure was traced to the Centaur boost pumps, but the cause was still unclear, thought likely to be either ice or debris. To reduce the chance of another similar failure, pre-launch procedures to verify Centaur's pumps were free and unobstructed were put in place. It took nearly four years to trace the cause of the failure to an improperly installed clip inside the liquid oxygen tank, which came loose and lodged in one of the boost pumps. Despite the failure, at least one important goal was accomplished in that the bulging Centaur payload shroud was proven to be aerodynamically stable in flight and had jettisoned properly and on schedule.
The next flight of the Titan IIIE was on December 10, 1974, carrying the Helios-A spacecraft. This mission was successful, as were all subsequent launches.
|11 February 1974
|23E-1||TC-1||Sphinx||Failure||Centaur LOX turbopump malfunction. RSO destruct at T+742 seconds.|
|10 December 1974
|23E-2||TC-2||Helios-A||Successful||First space probe to orbit closer to the Sun than Mercury.|
|20 August 1975
|23E-4||TC-4||Viking 1||Successful||Carried a lander that landed on Mars.|
|9 September 1975
|23E-3||TC-3||Viking 2||Successful||Carried a lander that landed on Mars.|
|15 January 1976
|23E-5||TC-5||Helios-B||Successful||Holds the record for fastest velocity relative to the Sun achieved by a space probe.|
|20 August 1977
|23E-7||TC-7||Voyager 2||Successful||Additionally boosted by a Star 37E upper stage.
Flew by Jupiter, Saturn, Uranus and Neptune, completing the Planetary Grand Tour. Now leaving the Solar System.
|5 September 1977
|23E-6||TC-6||Voyager 1||Successful||Additionally boosted by a Star 37E upper stage.
Flew by Jupiter and Saturn. Exited the Solar System heliosphere in 2012. Currently most distant object from Earth.
- Wade, Mark. "Titan". Encyclopedia Astronautica. Retrieved 2009-01-25.
- Krebs, Gunter. "Titan-3E Centaur-D1T Star-37E". Gunter's Space Page. Retrieved 2009-01-25.
- Krebs, Gunter. "Titan-3E Centaur-D1T". Gunter's Space Page. Retrieved 2009-01-25.
- Dawson, Virginia; Bowles, Mark (2004). Taming Liquid Hydrogen: The Centaur Upper Stage Rocket 1958-2002 (PDF). NASA. pp. 145–146.
Media related to Titan IIIE at Wikimedia Commons