Titan Flight History Page 3 of 3 Comprehensive Orbital Titan Failure List Date Vehicle ID Site Payload Failure Description Result# -------------------------------------------------------------------------------------------------------------------- 9/1/1964 Titan-3A 3A-2 CC LC20 Transtage 1 TS* He valv; 391s burn, 15s short FTO 10/15/1965 Titan-3C 3C-4 CC LC40 LCS 2/OV-2 1 TS fld before 3rd burn; OX leak; tumbled (LEO) 12/21/1965 Titan-3C 3C-8 CC LC41 LES 3,4/OV-2 3/Oscar 4 TS 3rd burn fld; stuck OX valve; no sep (GTO) 8/26/1966 Titan-3C 3C-12 CC LC41 IDCSP(8-14)/GGTS 2 Early P/L shroud sep; RSO at T+83s FTO 4/26/1967 Titan-3B 3B-5 V SLC4W KH-8 5 2nd stage malfunction FTO 11/6/1970 Titan-3C 3C-19 CC LC40 DSP 1 TS last burn failed, sat unusable sub-GEO (GTO) 2/16/1972 Titan-33B 3B-37 V SLC4W Jumpseat Agena Failed FTO 5/20/1972 Titan-24B 3B-35 V SLC4W KH-8 35 Agena Failed FTO 6/26/1973 Titan-24B 3B-43 V SLC4W KH-8 39 FTO (unknown cause) FTO 2/11/1974 Titan-3E 3E-1 CC LC41 Sphinx/Viking SD Centaur start failed; LOX boost pump FTO 5/20/1975 Titan-3C 3C-25 CC LC40 DSCS-2 5/DSCS-2 6 TS guidnce IMU failed, decyd 5/26 (LEO) 3/25/1978 Titan-3C 3C-35 CC LC40 DSCS-2 9/DSCS-2 10 2nd stg no start; Rng Safety (RSO) FTO 4/24/1981 Titan-34B 3B-60 V SLC4W Jumpseat Agena fail. 700 km apogee. 39377km plan (EEO) 8/28/1985 Titan-34D 34D-7 V SLC4E KH-11 7 1st stg shutdown after start, fuel leak FTO 4/18/1986 Titan-34D 34D-9 V SLC4E KH-9 20/SSF-D 6 SRM** expolded T+16s FTO 9/2/1988 Titan-34D 34D-3 CC LC40 Chalet 5 (Vortex 5) TS last burn failed, no GEO (GTO) 3/14/1990 Commrcl-T3 CT-2 CC LC40 Intelsat-6 3/Orbus-21S 2nd stg no sep frm Orbus (Titan design) (LEO) 8/2/1993 Titan-403A K-11 V SLC4E NOSS 13 + 3 Subsat SRM exploded T+101s FTO 10/5/1993 Titan-23G 23G-5 V SLC4W Landsat 6 Star-37 third stage failed FTO 8/12/1998 Titan 401A A-20 CC LC41 Vortex 2 (NRO) Expld T+41.3s, Pwr glitch caused pitchover FTO 4/9/1999 Titan 402B B-27 CC LC41 DSP 19 IUS% SRM-2 apogee failed due SRM-1 bad sep (GTO) 4/30/1999 Titan 401B B-32 CC LC40 Milstar 2 F1 Bad Centaur attitude control software (EEO) -------------------------------------------------------------------------------------------------------------------- Footnotes: * TS: Transtage (Hypergolic upper stage manufactured by Martin (Marietta) % IUS: Intertial Upper Stage (Two-unit solid motor upper stage manufactured by Boeing) ** SRM: segmented Solid Rocket Motor used on Titan 3C, 34D, 4xxA (manufactured by Alliant) # FTO: Failed to Orbit (EEO): Unintended Eliptical Earth Orbit (GTO): Unintended Geosynchronous Transfer Orbit (LEO): Unintended Low Earth Orbit References: Jonathan's Space Report Launch Vehicle Database "http://www.planet4589.org/space/lvdb/index.html" Encylopedia Astronautica "http://www.astronautix.com/" Gunter's Space Page "http://www.skyrocket.de/space" Stumpf, David K., "Titan II: A History of a Cold War Missile Program", The University of Arkansas Press, Fayetteville, Arkansas, 2000. TRW Space Log 1957-1996, TRW Space & Electronics Group, Redondo Beach, CA. Last Update 11-2-2003 by Ed Kyle