Accession Number : ADA162854
Title : Determining Thrust or Drag of a Rocket-Assisted Projectile from Doppler Trajectory Data
Descriptive Note : Technical rept
Corporate Author : ARMY ARMAMENT RESEARCH DEVELOPMENT AND ENGINEERING CENTER PICATINNY ARSENAL NJ ARMAMENT ENGINEERING DIRECTORATE
Personal Author(s) : Friedman, Eugene M. ; Amoruso, Michael J.
PDF Url : ADA162854
Report Date : NOV 1985
Pagination or Media Count : 22
Abstract : An analysis and associated computational technique were developed to measure rocket thrust using Doppler radar velocity trajectory data from rocket- assisted projectile firings. This technique was inserted into the ARDC standard six-degree-of-freedom flight simulation program, TRAJ5. During data reduction, the actual Doppler velocity from radar data is compared to the value predicted by the simulation. If they disagree, the thrust is adjusted until agreement occurs. The technique automatically determines rocket motor ignition and burnout times. The estimate of the specific impulse is also corrected. This method can also be used to estimate corrections to the drag coefficient of a projectile.
Descriptors : *COMPUTERIZED SIMULATION, *RADAR TRACKING, *DATA REDUCTION, *DRAG, *ROCKET ASSISTED PROJECTILES, *THRUST, *DOPPLER RADAR, COMPUTER PROGRAMS, FREE FLIGHT TRAJECTORIES, EXTENDED RANGE PROJECTILES, SPECIFIC IMPULSE, ROCKET ENGINES, FLIGHT SIMULATION, VECTOR ANALYSIS, TEST METHODS, COMPUTER PROGRAMMING, ALGORITHMS
Subject Categories : Active & Passive Radar Detection & Equipment
Ammunition and Explosives
Distribution Statement : APPROVED FOR PUBLIC RELEASE