Accession Number : AD0442728


Title :   X-22A TRI-SERVICE V/STOL AIRCRAFT


Descriptive Note : Monthly progress rept. no. 7, 1-30 June 1963


Corporate Author : BELL AEROSYSTEMS CO BUFFALO NY


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/442728.pdf


Report Date : 15 Jul 1963


Pagination or Media Count : 55


Abstract : Final design resolutions are being made which incorporate revisions required for the improved longitudinal and directional stability. Flight control system design weight has been established. Further weight control studies are continuing. Wind Tunnelmodel tests have been resumed on the 1/5 scale powered model and are continuing with modified controls. The second series of tests on the 1/6 scale unpowered model were started. TESTING OF Wing Compression Test Panels has been started.


Descriptors :   *VERTICAL TAKEOFF AIRCRAFT , AIRCRAFT MODELS , AIRFRAMES , COCKPITS , CONTROL , ELECTRICAL EQUIPMENT , FLUTTER , GAS TURBINES , HUMANS , HYDRAULIC EQUIPMENT , LANDING GEAR , MAINTAINABILITY , PERFORMANCE(ENGINEERING) , RESEARCH MANAGEMENT , SIMULATION , STABILITY , STRUCTURAL PROPERTIES , SYSTEMS ENGINEERING , WEIGHT


Subject Categories : V/STOL


Distribution Statement : APPROVED FOR PUBLIC RELEASE