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Aerodynamic characteristics of a tubeflight vehicle support system
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.... ,.- - ' - " " - . - - .. - _ .. - - .... " . ' -- ~ . - - - - - _ . 45 .,tFt tl: :~ r…
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46 •• - _ . < -"""- _.-", - - .. ," .. - ."- - H-I+HH-1+H -- .- .. -.…
An inflight data recording system for tubeflight vehicles
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PROJECllUBEFlIGHl
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TN PT 6907 ~ AN INFLIGHT DATA RECORDING SYSTEM FOR TUBEFLIGHT VEHICLES by Dennis I. Powell Robert E. Duffy This research…
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SUMMARY This report is concerned with the technique of measuri.ng the attitude of a tubeflight vehicle ~lile it is traversing…
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INTRODUCTION , The testing of a small-scale model tubefli~ht vehicle has been conducted in the T-2 facility constructed by…
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2 DATA RECORDING SYSTEM Some possible solutions to the problem of obtaining data from which vehicular moti.on can be…
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3 (G. M. Giannini & Co. Linear Accelerometers, Model 3858, ± 2.5G's) comprise the roll sy;stem. They are mounted…
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4 in the telemetry system. Mounted on the vehicle is a sheet of soft rubber wrapped around the fuselage and firmly attached…
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system tests (called for in Step 2), The system test,outlined in Appendix A, should also be tested at a few locations along…
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6 vehicle which lie in a diametrical plane are discernible. Motions associated with yaw'and/or transverse displacement…
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illustrated using Figure 14, which is a representation of one card. The basic card consists of 80 columns; therefore, the…
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8 TIM I Card TIMLON (J) TIM Cards in Chronological Order TUnpOS (J) TIM Cards in Chronological Order FOWINT I Card…
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(see Figure 16) PICHV}~(L) 111'--'1-117';'(-· ) "II ·.,"',nlI1~(I _. 1) r. .. t…
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ROLL VARIABLES Roll Angle Roll Velocity Roll Acceleration ROLLAC (N) - lIeasu.:ccc1 10 Integration based on average…
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'I'lF' !:'J) 0 ("[ J') .... J .. ,J _ .. '" LONGITUDINAL VARIABLES (from Photocell…
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12 AIPVI'" (I'Tr) .\. v.!. 1. ,'~.'" OUTPUT The printed output from the program has been…
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The program was tested for reliability with a rather rigorous specified flight profile. Table VI is a listing of the equations…
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heaving, the output with the system in its present state would indicate a pure heave (see Figure 18). From stability theory,…
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Longitudinal Loc8.tion Longitudinal Velocity Lonrritudinal Acceleration r.Joll~it1.1dinal Location I ... on[~itudinal…
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'X'iill V;; I I Lon:situdinal Acceleration (uncorrected for pitch) ;1011 Acceleration Heave of Forvard Support Fad…
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AIRVEL( ) AVLGAC( ) AVRLAC( ) CGIHIT CGFORH CGPROX OGRT~AR FOHACH( ) FOVELO( ) FOfnNtl' FQ':-:'PRX…
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PIcnAce PICH.AN( PICHVE P'")F'SS'~( .'"~ .... ,,~., 1: PRSINrr pP'::'P:,\tf…
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'rum TJ.l.ILOH( ) '£0:..'1118 TO~L'?RS TUBACC( ) TUBEAC( ) 'rUI3EAA( ) rl'UBEPO( ) '…
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