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NASA Technical Reports Server (NTRS) 19930019535: NEP Space Test Program Objective PDF

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Preview NASA Technical Reports Server (NTRS) 19930019535: NEP Space Test Program Objective

NEP 5Dace Test Program Objective ~ "-. ~I\ ~ ~ ~ \J ~ The Objective Of The NEP Space Tes To Launch A NEP S .. ... To Septembet 15.1992 NEPSp.oe Space Technology Research Vehicle. 'I 1 Pial, - Experiments • of recent advances in the PV area -. . ul "industry su If -- Increase cooperation SA LeRC ORA - Power Panels ----tl -- Useful "sDace hardware" exp . nt s solar cell technology CH cells in a hostile environment ... __ • outslae co - ---41 - Ground testin -- ConTI of space data and other ground testing -- Partici US-ESA calibration effo '"', . . G Oa a Flow 128xS12x12 Xmage ______________________ ~ ~~ 256xS12x12 xmage amples/sec IR D to b riz d cro 1--'" rocessor He der RAM Status Bit Command Mi rror Tape #1 Tape #2 Uplink Control Control Control Data Downlink ceo Microproces or Trigg rs Re dout . Data Control rdwar wri t xm g plus B d r dat to ape corder. Data Control witch s xm 9 Buffer ceo from to T p • sor summarizes from tape M~croproc Low-rate image bu fers, samples lR, and writes data (1200 baud) this data with time- t amp into Medium-Rate Beader RAM. Data (MRD) ~LOCkheed Glow Avionics Bloc Drblter Hltchhlker-M (IS& '. PWR TRPl alCORDlRS .o J) .2' .. j~ ~ MRIN Dt DATA CNTl/ST ATUS ~ PWR .. TIMING lOA FUU UI. II I I PTa MET .. .1) P,T Dedicated DATA J • l '~ 4r- J J TSAWlKITBCAHCEKSSI .. aUIONICS lHp.rlm.nt ~ CNTl SSP Proc ••••r UNIT - PWR l UPLINK CMOS .. (OlP' J l .r T/CJ COMMANDS .. ~ PSP ~ N2 Mirror 6a. 6a. DOWNLINK __ DATA - DATA Uelu. Ualu. PDI - THERMISTORS (3) • IMPORTANCE OF COMBINING SKIRT WITH EISG (con't) • SKIRT will allow EISG to measure other contributors to the infrared glow: OH, NO+, •• _" •.. • SKIRT will obtain data during both day and night sides '. of orbits, thereby enhancina EISG niaht-o ••• ~~~ 1r ..... • Comparing SKIRT data from STS-39 and STS-62 will show the dependence of the glow on· · activity cycle. • EISG/SKIRT will expand and enhance the technolog base Dertainina to shuttle glo ••. '-, IMPORTANCE OF COMBINING SKIRT WITH EISG • Only by including SKIRT as part of EISG will it be possible to investigate all aspects of the alow Drocess. SKIRT aives IR spectroscopic cove • The elliptical orbits planned for STS-62 will provide unique opportunity to measure the IR, visi_._, glow as a function of altitude. Altitude informatio was not obtained by S • EISG nitrogen gas releases will Drovide the first combined IR, vis· plays in the alow chemis •• 1J • ...... ~ .,. THE ROLE OF INFRARED SPECTRA IN INVESTIGATING THE GLOW PROCESS • Spacecraft-atmospheric interaction involves three reac s . 1) 2 + 0 -> NO + N 2) Osurfac- ..... . - 3) Nsurface + N -> N2* • Reaction 1) is monitored by observing NO spectral emisslo • s s ed by S • Reactions 2) and 3) are monitored by observing N02* and N 2* spectral emissions in the vis· ultraviolet. resDecti. _ ••• • Only by observing spectra in all three regimes -IR visible, and UV • can t studie"". ........., 1.2~------------------------------------------------------------------~ 1.0 ,t ~ III 2.9 microns 1 0.8 1 • ~ 4.5 microns a 5.3 microns 0.6 ....... -+- cos squared .. -I W 0 Z - c( 0.4 C a~: 0.2 0.0 -0.2 0 20 40 60 80 100 RAM ANGLE degrees Figure 36. 2.9 pm, 4.5pm, and 5.5 pm Glow Intensities VB Ram Angle.2S ......., : Quiescent Shuttl 10 (S'gnal Aver."ed) Thruster Shuttle Glow • !) ., Co • u ., C' ...... I ~ E r~:~iimb OH -- .. ..• ... ••• I •• I .• UII

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