Titan IIIB

Last updated
"Titan 3B Launch" . Aviation Week and Space Technology. McGraw Hill Publishing Company. 8 August 1961. p. 29. Retrieved 27 July 2021.
  • "Titan 23B". www.astronautix.com. Archived from the original on December 27, 2016. Retrieved 2021-08-27.
  • "History of Satellite Reconnaissance Volume 5, Management of NRP" (PDF). US National Reconnaissance Office. Archived from the original (PDF) on 2 April 2012. Retrieved 19 September 2011.
  • Perry, Robert, A History of Satellite Reconnaissance (PDF), vol. IIIA, US National Reconnaissance Office, pp. 291–2, archived from the original (PDF) on 2012-09-16, retrieved 2012-06-04
  • Wade, Mark. "Titan 33B". Encyclopedia Astronautica. Archived from the original on December 30, 2003. Retrieved 19 September 2011.
  • Wade, Mark. "Titan 24B". Encyclopedia Astronautica. Archived from the original on September 4, 2003. Retrieved 19 September 2011.
  • Titan IIIB
    Titan 23B.jpg
    Titan 23B launching KH-8 reconnaissance satellite from Vandenberg AFB, CA. (USAF)
    FunctionMedium launch vehicle
    Manufacturer Martin
    Country of originUnited States
    Size
    Height45 m (148 ft)
    Diameter3.05 m (10.0 ft)
    Mass156,540 kg (345,110 lb)
    Stages3
    Capacity
    Payload to LEO
    Mass3,300 kg (7,300 lb) (23B)
    Associated rockets
    Family Titan
    Launch history
    StatusRetired
    Launch sites SLC-4W, Vandenberg AFB
    Total launches68
    Success(es)62
    Failure(s)4
    Partial failure(s)2
    First flight29 July 1966
    Last flight12 February 1987
    First stage (Titan 23B/33B)
    Powered by2 LR87-AJ-5
    Maximum thrust1,913 kN (430,000 lbf)
    Burn time147 seconds
    Propellant N2O4 / Aerozine 50