Titan IIIB

Titan IIIB

Titan 23B launching KH-8 reconnaissance satellite from Vandenberg AFB, CA. (USAF)
Function Medium launch vehicle
Manufacturer Martin
Country of origin United States
Size
Height 45m (147.00 ft)
Diameter 3.05m (10 ft)
Mass 156,540kg (345,110 lb)
Stages 3
Capacity
Payload to LEO 3,000kg (7,500 lb (23B))
Associated rockets
Family Titan
Launch history
Status Retired
Launch sites SLC-4W, Vandenberg AFB
Total launches 68
Successes 63
Failures 4
Maiden flight 29 July 1966
Last flight 12 February 1987
First stage (Titan 23B/33B)
Engines 2 x LR87-AJ-5
Thrust 1,913 kN (430,000 lbf)
Burn time 147 seconds
Fuel A-50 hydrazine/N2O4
Second stage
Engines 2 x LR91-AJ-5
Thrust 445 kN (100,000 lbf)
Burn time 205 seconds
Fuel A-50 hydrazine/N2O4
Third stage - Agena
Engines 1 x Bell XLR81-BA-9
Thrust 71.1 kN (16,000 lbf)
Burn time 240 seconds
Fuel N2O4/UDMH

Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle, modified by the addition of an Agena upper stage. It consisted of four separate rockets. The Titan 23B was a basic Titan II with an Agena upper stage, and the Titan 24B was the same concept, but using the slightly enlarged Titan IIIM rocket as the base. The Titan 33B was a Titan 23B with the Agena (which had a smaller diameter than the Titan) enclosed in an enlarged fairing, in order to allow larger payloads to be launched. The final member of the Titan IIIB family was the Titan 34B which was a Titan 24B with the larger fairing used on the Titan 33B.

Contents

Titan 23B

Titan 23B is a medium-lift space launch vehicle used to carry payloads for the Air Force. The Titan 23B was launched from Vandenberg AFB, Calif. Its main payload was the GAMBIT (KH-8 reconnaissance) satellites.

Features

The Titan 23B space launch vehicle was a three-stage liquid fueled booster, designed to provide a small-to-medium weight class capability. It is able to lift approximately 3,000 kg (7,500 lb) into a polar low-Earth circular orbit. The first stage consists of a ground ignited LR87 liquid propellant rocket, while the second stage consists of an LR91 liquid propellant rocket. The third stage is an Agena D XLR81-BA-9 liquid propellant rocket.

Various models of this Titan/Agena D rocket were called, "Titan 23B", "Titan 24B", "Titan 33B" and "Titan 34B".

Background

The Titan rocket family was established in October 1955, when the Air Force awarded The Martin Company a contract to build an intercontinental ballistic missile (ICBM). It became known as the Titan I, the nation’s first two-stage ICBM and first underground silo-based ICBM. More than 140 Titan II ICBMs, once the vanguard of America’s strategic deterrent force, were built. Titan IIs also were flown in NASA’s Gemini manned space program in the mid-1960s. The Titan 23B is a derivative of the Titan II vehicle with an Agena D upper stage added.

Titan 24B

The Titan 24B differed from the Titan 23B in that the stretched Titan IIIM core was used in place of the original Titan II core.

Titan 33B

The Titan 33B was a Titan 23B with a larger payload fairing, which sat atop the second stage, enclosing the Agena, rather than atop the Agena, as had been flown on the 23B and 24B.

Titan 34B

The Titan 34B was a Titan 24B, modified by the addition of the larger fairing used on the Titan 33B.

Failures

Titan IIIB rockets suffered four outright failures, and a partial failure. The first failure occurred on 26 April 1967, when the second stage of a Titan III(23)B lost thrust during the launch of a Gambit 3 satellite. The next launch, on 20 June 1967 was a partial failure; due to a problem with the protective skirt on the second stage, a lower-than-planned orbit was achieved.[1]

On 16 February 1972, a Titan III(33)B failed to achieve orbit carrying a Jumpseat satellite.[2] Another failure occurred later the same year, when on 20 May a Titan III(24)B failed to achieve orbit with another Gambit 3. Another Titan III(24)B failed to place a Gambit 3 into orbit on 26 June 1973, this time because of the Agena malfunctioning.[3]

See also

References

  1. ^ "History of Satellite Reconnaissance Volume 5, Management of NRP". US National Reconnaissance Office. http://www.nro.mil/foia/declass/GAMHEX/GAMBIT/2.PDF. Retrieved 19 September 2011. 
  2. ^ Wade, Mark. "Titan 33B". Encyclopedia Astronautica. http://www.astronautix.com/lvs/titan33b.htm. Retrieved 19 September 2011. 
  3. ^ Wade, Mark. "Titan 24B". Encyclopedia Astronautica. http://www.astronautix.com/lvs/titan24b.htm. Retrieved 19 September 2011. 

External links