Accession Number : AD0875878
Title : Side Force Measurement for LANCE Engine Testing.
Descriptive Note : Test evaluation rept.,
Corporate Author : ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL TES T AND EVALUATION DIRECTORATE
Personal Author(s) : Presson, A. W.
Report Date : 07 JUL 1970
Pagination or Media Count : 36
Abstract : The report deals with the LANCE Engine Test Stand capability to measure the side force developed by thrust vector control value action. The basic calibration was supplemented and validated by a group of dynamic calibrations involving the application of deadweight step functions during booster phase of the engine system tests. A limited sample of such tests performed at ambient temperature conditions along with two hot temperature and one cold temperature conditioned tests is examined. (Author)
Descriptors : (*LIQUID PROPELLANT ROCKET ENGINES, CAPTIVE TESTS), (*SURFACE TO SURFACE MISSILES, LIQUID PROPELLANT ROCKET ENGINES), THRUST VECTOR CONTROL SYSTEMS, CALIBRATION, TEMPERATURE, TEST EQUIPMENT.
Subject Categories : Surface-launched Guided Missiles
Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE