Tt?& DAC-58065 . # STUDY OF THRUST-VECTOR-CONTROL SYSTEMS FOR LARGE. SOLID-FUELED LAUNCH VEHICLES e 3 COMPARATIVE AVOLUME 4 1:f ;* # UMMARY 6 q NOVEMBER 1967 /o(=q By…
P N87- 16342 A MECHANISM FOR PRECISE LINEAR AND ANGULAR ADJUSTMENT UTILIZING FLEXURES* J. R. Ellis# This paper describes the design and development of a mechanism for pre-…
i ^ f "^ V NASA CONTRACTOR REPORT 166389 f ^!« .;,v . -CR-166389) A,ERQNLA$TIC STABILITY BLADES USING FINITE FLEMENT ANALY (Stanford Univ.) 119 p HC ln6/MF A01 C S…
^ / * ? 4 > > / GAS TURBINE LABORATORY DEPARTMENT OF AERONAUTICS AND ASTRONAUTICS MASSACHUSETTS INSTITUTE OF TECHNOLOGY CAMBRIDGE, MA 02139 A FINAL REPORT ON NASA GRANT…
/ ANALYSIS CONF' IGURATION G. A. Richards, et a! AD-756 470 AND DESIGN OF SPECIAL ANTENNA Ohio State University Prepared for: Ballistic Research Laboratories November…