An Entity of Type: Thing, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

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.

Property Value
dbo: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)
dbo:thumbnail
dbo:wikiPageID
  • 70746778 (xsd:integer)
dbo:wikiPageLength
  • 14321 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1119928833 (xsd:integer)
dbo:wikiPageWikiLink
dbp:burnTime
  • 135.7
dbp:caption
  • Titan IV-B with 2 SRMU boosters (en)
dbp:casing
  • Composite (en)
dbp:chamberPressure
  • 859.5
dbp:designer
dbp:diameter
  • 3.2m (en)
dbp:dryWeight
  • 80611.0
dbp:fuel
dbp:gimbal
  • 6 (xsd:integer)
dbp:imageSize
  • 300 (xsd:integer)
dbp:length
  • 34.26 m (en)
dbp:manufacturer
dbp:name
  • Solid Rocket Motor Upgrade (en)
dbp:nozzleRatio
  • 15.700000 (xsd:double)
dbp:predecessor
dbp:purpose
  • Solid rocket booster (en)
dbp:status
  • Retired (en)
dbp:thrust
  • 6.410000 (xsd:double)
dbp:type
  • solid (en)
dbp:wikiPageUsesTemplate
dcterms:subject
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)
rdfs:label
  • Solid Rocket Motor Upgrade (en)
owl:sameAs
prov:wasDerivedFrom
foaf:depiction
foaf:isPrimaryTopicOf
is foaf:primaryTopic of
Powered by OpenLink Virtuoso    This material is Open Knowledge     W3C Semantic Web Technology     This material is Open Knowledge    Valid XHTML + RDFa
This content was extracted from Wikipedia and is licensed under the Creative Commons Attribution-ShareAlike 3.0 Unported License