Accession Number : ADA124482


Title :   A Gasdynamic Analysis of a High Speed Pneumatic Missile Launching System.


Descriptive Note : Final rept. 15 Apr-1 Aug 82,


Corporate Author : NAVAL OCEAN SYSTEMS CENTER SAN DIEGO CA


Personal Author(s) : Schneider,S P


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a124482.pdf


Report Date : 30 Sep 1982


Pagination or Media Count : 56


Abstract : This paper presents an analysis of a high speed compressed air missile launching system, consisting of a reservoir, valve, and launch tube. Simplifying assumptions are discussed and made, a model is determined, and its numerical solution using FORTRAN is presented. (Author)


Descriptors :   *MATHEMATICAL MODELS , *GUIDED MISSILE LAUNCHERS , *GAS DYNAMICS , HIGH VELOCITY , NUMERICAL ANALYSIS , FORTRAN , MATHEMATICAL ANALYSIS , VALVES , EQUATIONS , COMPRESSED AIR


Subject Categories : Guided Missile Launching and Basing Support
      Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE