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The Solid Rocket Motor Upgrade (SRMU) was a solid rocket motor that was used as a booster on the Titan IVB launch vehicle. Developed by Hercules (later ATK), it was intended to be a high-performance, low-cost upgrade to the UA1207 boosters previously used on Titan IV.
Most of the Titan rockets were the Titan II ICBM and their civilian derivatives for NASA.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 (NTO) for its oxidizer and Aerozine 50 (a 50/50 mix of hydrazine and unsymmetrical dimethylhydrazine (UDMH) instead of the liquid oxygen and RP-1 propellant of the Titan I.
The Inertial Upper Stage (IUS), originally designated the Interim Upper Stage, was a two-stage, solid-fueled space launch system developed by Boeing for the United States Air Force beginning in 1976 [4] for raising payloads from low Earth orbit to higher orbits or interplanetary trajectories following launch aboard a Titan 34D or Titan IV rocket as its upper stage, or from the payload bay of ...
Final flight of Titan IIIC 11 May 18:45 Titan III(23)D: 23D-24 VAFB SLC-4E: LEO: Success OPS-5642 SSF-D-4: 30 October 04:05 Titan 34D/IUS: 4D-5 34D-1 CCAFS LC-40: GSO: Success OPS-9446 OPS-6451 DSCS III-A1: First flight of Titan 34D 17 November 21:22 Titan III(23)D: 23D-23 VAFB SLC-4E: LEO: Success OPS-9627 Final flight of Titan IIID
A retired Titan II missile, repainted as GLV-3 12558 (Gemini 3), is on display at KSC Rocket Garden since 2010. [8] Another retired Titan II missile, repainted as GLV-9 12564 (Gemini 9A), is on display at the Stafford Air & Space Museum. [9] A Gemini-Titan II full-scale replica was erected for the 1964 New York World's Fair.
Titan IVA K-11 moments before the August 1993 failure. On August 2, 1993, Titan IV K-11 lifted from SLC-4E carrying a NOSS SIGNIT satellite. Unusually for DoD launches, the Air Force invited civilian press to cover the launch, which became more of a story than intended when the booster exploded 101 seconds after liftoff.
T62 Titan The direct drive main production version. T62T-2 80 hp (60 kW) at 56,700 turbine rpm for Boeing-Vertol CH-47A Chinook helicopters. [1] T62T-2A 95 hp (71 kW) at 56,700 turbine rpm for Boeing-Vertol CH-47B / C Chinook helicopters. [1] T62T-11 80 hp (60 kW) at 56,700 turbine rpm for Boeing-Vertol CH-46A Sea Knight helicopters. [1] T62T-12
Flux F through a surface, dS is the differential vector area element, n is the unit normal to the surface. Left: No flux passes in the surface, the maximum amount flows normal to the surface.
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