Category:Inertial Upper Stage

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The Inertial Upper Stage (IUS) is a two-stage solid-fueled booster rocket developed by NASA and the U.S. Air Force for the launching of large payloads from either a Titan III (later Titan IV) rocket or from the payload bay of the Space Shuttle.

<nowiki>Inertial Upper Stage; Inertial Upper Stage; Inertial Upper Stage; Inertial Upper Stage; Inertial Upper Stage; Inertial Upper Stage; IUS; Inertial Upper Stage; 慣性上段ロケット; Inertial Upper Stage; Inertial Upper Stage; Inertial Upper Stage; Inertial Upper Stage; IUS; Inertial Upper Stage; 慣性上層節; Inertial Upper Stage; Inertial Upper Stage; dvostopenjska nosilna raketa na trdno gorivo, ki jo je razvilovAmeriško vojno letalstvo; Modul von Boeing, um Satelliten in eine höhere Umlaufbahn zu bringen; two-stage solid-fueled booster rocket developed by the U.S. Air Force; Étage de propulsion spatiale; two-stage solid-fueled booster rocket developed by the U.S. Air Force; IUS; インターナル・アッパー・ステージ; Interim Upper Stage; IUS; 慣性上升助推器; Interim Upper Stage; IUS; SSB-7</nowiki>
Inertial Upper Stage 
two-stage solid-fueled booster rocket developed by the U.S. Air Force
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Instance of
  • rocket model
Subclass of
Country of origin
Has part(s)
  • Orbus-21 (1)
  • Orbus-6 (2)
Manufacturer
Service entry
  • 1982
Service retirement
  • 2004
Diameter
  • 2.9 m
Height
  • 5.17 m
Authority file
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Subcategories

This category has the following 12 subcategories, out of 12 total.

C

D

G

M

T

U