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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. Wound from carbon-fibre-reinforced polymer and burning a hydroxyl-terminated polybutadiene-bound ammonium perchlorate composite propellant, it was an ambitious upgrade building on Hercules' experience developing a filament-wound case for the Space Shuttle SRB. Originally intended to fly in 1990, it instead first flew in 1997 due to a protracted development and lack of demand. The SRMU performed successfully on all of its flights.

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rdfs:label
  • Solid Rocket Motor Upgrade (en)
rdfs:comment
  • 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. Wound from carbon-fibre-reinforced polymer and burning a hydroxyl-terminated polybutadiene-bound ammonium perchlorate composite propellant, it was an ambitious upgrade building on Hercules' experience developing a filament-wound case for the Space Shuttle SRB. Originally intended to fly in 1990, it instead first flew in 1997 due to a protracted development and lack of demand. The SRMU performed successfully on all of its flights. (en)
name
  • Solid Rocket Motor Upgrade (en)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/140603-F-IO108-001.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/160323-F-IO108-002.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/160323-F-IO108-003.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/160323-F-IO108-005.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/160323-F-IO108-007.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/160323-F-IO108-008.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/Titan_IVB_core_vehicle_arrive_at_the_pad_at_Launch_Complex_40.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/Titan_IVB_launch_with_Cassini-Huygens_on_Board.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/Titan_IVB_Centaur_launching_ELINTspy_satellite.jpg
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thrust
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caption
  • Titan IV-B with 2 SRMU boosters (en)
designer
diameter
  • 3.2m (en)
fuel
image size
length
  • 34.26 m (en)
manufacturer
predecessor
purpose
  • Solid rocket booster (en)
status
  • Retired (en)
type
  • solid (en)
has abstract
  • 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. Wound from carbon-fibre-reinforced polymer and burning a hydroxyl-terminated polybutadiene-bound ammonium perchlorate composite propellant, it was an ambitious upgrade building on Hercules' experience developing a filament-wound case for the Space Shuttle SRB. Originally intended to fly in 1990, it instead first flew in 1997 due to a protracted development and lack of demand. The SRMU performed successfully on all of its flights. (en)
burn time
casing
  • Composite (en)
chamber pressure
dry weight
gimbal
nozzle ratio
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