Accession Number : AD0861348

Title :   Maximum Range Capability of 'D' and 'E' Series Atlas with and without Propellant Utilization Control,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Rose, R.

Report Date : 21 MAR 1961

Pagination or Media Count : 30

Abstract : The purpose of this report is to indicate the range capability for D and E series Atlas missiles, with and without PU control, as determined from a Monte Carlo statistical study. (Author)

Descriptors :   (*SURFACE TO SURFACE MISSILES, GUIDED MISSILE TRAJECTORIES), (*GUIDED MISSILE TRAJECTORIES, RANGE(DISTANCE)), (*PROPELLANT BURN OUT, OPTIMIZATION), LIQUID PROPELLANT ROCKET ENGINES, PROPELLANT TANKS, PROPELLANT CONTROL, PROBABILITY, MONTE CARLO METHOD, LIQUID ROCKET PROPELLANTS.

Subject Categories : Guided Missile Traj, Accuracy and Ballistics
      Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE