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  2. File:The Burton case (IA b22315597).pdf - Wikipedia

    en.wikipedia.org/wiki/File:The_Burton_case_(IA_b...

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  3. Space Launch System core stage - Wikipedia

    en.wikipedia.org/wiki/Space_Launch_System_core_stage

    LH 2 tank of CS-2 after thermal protection system (TPS) application. The engine section receives a different thermal protection system application from the rest of the stage. With higher predicted heat loads than the other structures, it is covered in sheets of P50 cork, a composite substance of ground cork and phenolic binders.

  4. Long March 2 - Wikipedia

    en.wikipedia.org/wiki/Long_March_2

    Long March 2 was the original model in the Long March 2 rocket family, which was derived from China's first ICBM, the DF-5. The development work began in 1970. The first rocket was launched on November 5, 1974, [1] but the launch failed. After the failed first launch of Long March 2, its design was slightly modified and designated as Long March 2A.

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  7. File:V-2 rocket diagram (with English labels).svg - Wikipedia

    en.wikipedia.org/wiki/File:V-2_rocket_diagram...

    The following 34 pages use this file: Blizna V-2 missile launch site; History of rockets; Rocket U-boat; Wernher von Braun; User:Yunshui/Wikipedia is not rocket science; User talk:TomStar81/Archive; User talk:TomStar81/Archive 7; User talk:TomStar81/Archive 8; Wikipedia:Featured picture candidates/Ballistic Missile diagram

  8. File:Stratolaunch comparison.svg - Wikipedia

    en.wikipedia.org/wiki/File:Stratolaunch...

    This file contains additional information, probably added from the digital camera or scanner used to create or digitize it. If the file has been modified from its original state, some details may not fully reflect the modified file.

  9. RUM-139 VL-ASROC - Wikipedia

    en.wikipedia.org/wiki/RUM-139_VL-ASROC

    The vertical launch missile first became operational in 1993, with more than 450 having been produced by 2007. It is 4.5 meters (15 ft) in length, with a firing range of about 11.8 nm or 22 kilometers (24,000 yd). [2] Beginning in 1996, the missile was replaced by the newer RUM-139A and subsequently the RUM-139B.