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  • NASA TECHNICAL NOTE NASA TNArizona State University

    nasa technical note nasa tn d-1868 00 40 i ithru) "n65 12201 8 (accession number1 i f p 2 > ow .t icodei i (page91 4 icateooryi (nasa cr or tmx or ad number) i a review of photography of the earth from sounding rockets and satellites by paul d. lowman jr. goddard space flight center greenbelt m d gpo price ots price(s) #

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  • NASATechnical Notes

    1869 Pomona Road Unit A. Corona CA 92880. . aeroinstruments sbcglobal. (Aerophysics acquired much of the intellectual property from Task/Able) Triumph Aerospace Force Measurement Systems. AIAA Recommended Practice for Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (R) AIAA

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  • NASA TECHNICAL NOTE NASA TN D-6082

    NASA TECHNICAL NOTE LUNAR LANDMARK LOCATIONSAPOLLO 8 10 11 AND 12 MISSIONS by Gary A. Ransford Wilbur R. Wollenhaupt and Robert M. Bizzell Ma1zned Spacecraft Center Houston Texas 77058 NASA TN D-6082

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  • I NASA TECHNICAL NOTE NASAibiblio

    I NASA TECHNICAL NOTE NASA TN D-8249 0- .d N 00 n z c e APOLLO EXPERIENCE REPORTGUIDANCE AND CONTROL SYSTEMS Raymond E. Wilson Jr. Lylzdon B. Johizson Space Center Houston Texas 77058 NATIONAL AERONAUTICS AND

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  • Home NASA Technical Standards System (NTSS)

    The NASA Technical Standards System (NTSS) is a key element of the NASA Technical Standards Program (NTSP) sponsored by the Office of the NASA Chief Engineer. It provides access to technical standards from specifically contracted Standards Developing Bodies at no direct cost to the user via electronic subscription delivery and on a pay-per

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  • TECHNICAL NOTE NASA TN D- -- I

    nasa cr) h 00 t n z c 4 c/) 4 z technical note nasa tn d- p. i --analysis of sextant navigation measurements during lunar module rendezvous by t. b. murtagh manned spacecmfl center houston texas national aeronautics and space administration washington d. c. february 1967

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  • April 1969 NASA TECHNICAL NOTE BOOK SCALED LUNAR

    Details aboutApril 1969 NASA TECHNICAL NOTE BOOK SCALED LUNAR MODULE NASA TN-D-5051. April 1969 NASA TECHNICAL NOTE BOOK SCALED LUNAR MODULE NASA TN-D-5051.

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  • NASA TECHNICAL NOTE NASA TN D-2976

    NASA TECHNICAL NOTE NASA TN D-2976 ONE-DIMENSIONAL NUMERICAL ANALYSIS OF THE TRANSIENT RESPONSE OF THERMAL PROTECTION SYSTEMS by Robert T. Swanr Claud M. Pittman and James C. Smith Langley Research Center Langley Station Hampton Va. 61 74

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  • TECHNICAL NOTE NASA TJN D-5869klabs

    NASA c14 o 00 Ih I icI z c TECHNICAL NOTE NASA-TJN D-5869 DESCRIPTION AND PERFORMANCE OF THE SATURN LAUNCH VEHICLE S NAVIGATION GUIDANCE AND CONTROL SYSTEM by WuZter Huenssermunn George C. MurshuZZ Space FZight Center MurshuZZ Spuce Flight Center AZu 35 812

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  • NASA TECHNICAL NOTE -- TN E6723

    NASA TN E6723 c.1 NASA TECHNICAL NOTE -- = -= LOAN COPY RETURN 72m 2 KIRTLAND AFB N. M. a0- W= p AFWL (DOLJL) tn= -F--2 E APOLLO EXPERIENCE REPORTS-BAND SYSTEM SIGNAL DESIGN AND ANALYSIS Harold R. Rosenberg Editor Manned Spacecraft Center i Houston Texas 77058 .A " 4 1.. L 1 - -. s. . 9-

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  • TECHNICAL NOTE NASA geometry

    asa technical note nasa tn 015541 " i i i a case f copy infinite periodic minimal surfaces without self-intersections cambridg mass. 02139 i- national aeronautics and space administration washington d. c. may 1970 i. .. . 1- --

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  • NASA TECHNICAL NOTE 1 NASA TN D-2603

    nasa technical note co no cm 1 nasa tn d-2603 distribution statement a approved for public release distribution unlimited stress-intensity factors for single-edge-notch specimens in bending or combined bending and tension by boundary collocation of a stress function - ttt

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  • NASA TECHNICAL NOTE --. NASA TN c

    nasa technical note nasa tn d-6002 c r i -4 -0 -m -=- effects of a retronozzle located at the apex of a 140° blunt cone at m-ach numbers of 3.00 4.50 and 6.00 13 b by robert j. mcghee lungley resemch center national aeronautics and space administration washington d. c. january 1971

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  • NASA TECHNICAL NOTE NASA TNArizona State University

    nasa technical note nasa tn d-1868 00 40 i ithru) "n65 12201 8 (accession number1 i f p 2 > ow .t icodei i (page91 4 icateooryi (nasa cr or tmx or ad number) i a review of photography of the earth from sounding rockets and satellites by paul d. lowman jr. goddard space flight center greenbelt m d gpo price ots price(s) #

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  • NASA TECHNICAL NOTE NASA TN D-6575

    nasa technical note nasa tn d-6575 ln h m 4 a summary of spin technology as related to light i general-aviation airplanes i by james s. bowman jre langley research center hampton va 23365 i national aeronautics and space administration washington d. c. december 1971

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  • Apollo Experience Reportsklabs

    Manned Spacecraft Center NASA NASA Technical Note TN D-6847 June 1972 tn-d6847_apollo_abort_planning.pdf Abstract Definition of a practical return-to-earth abort capability was required for each phase of an Apollo mission. A description of the basic development of the complex Apollo abort plan is presented in this paper.

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  • NASA Parawing Research2e5

    These models are described in two NASA technical reports NASA TN D-5936 and NASA TN D-5965. A list of technical reports including these can be found on the NASA Parawing Reports page. NASA Parawing models 1-10 NASA Parawing models 1-10 are described in technical report NASA TN D-5936 found at the NASA Technical Reports Server.

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  • NASA TECHNICAL NOTE NASA TN 0-7919

    NASA TECHNICAL NOTE APOLLO EXPERIENCE REPORTCREW STATION INTEGRATION Volume II -Crew Station Displays and Controls William A. Langdoc and Dale A. Nussman Lyndon B. johnson Space Center Houston Texas 77058 NASA TN 0-7919 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON D. C. • APRIL 1975

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  • NASADryden Technical Report Server

    Report Number NASA-TN-D-6800. Performing Organization NASA Dryden Flight Research Center Edwards CA. Availability Format (s) on-line PDF (12 838 KBytes) Report Date June 1972. No. Pages 371. FLIGHT-DETERMINED CHARACTERISTICS OF AN AIR INTAKE SYSTEM ON AN F-111A AIRPLANE Technical Note.

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  • NASA TECHNICAL NOTE NASA TNArizona State University

    nasa technical note nasa tn d-1868 00 40 i ithru) "n65 12201 8 (accession number1 i f p 2 > ow .t icodei i (page91 4 icateooryi (nasa cr or tmx or ad number) i a review of photography of the earth from sounding rockets and satellites by paul d. lowman jr. goddard space flight center greenbelt m d gpo price ots price(s) #

    Get Price
  • April 1969 NASA TECHNICAL NOTE BOOK SCALED LUNAR

    SCALED LUNAR MONDULE. NASA TECHNICAL MANUAL. NASA TN D-5051. April 1969. 11" x 8 42 pages.

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  • NASA TECHNICAL NOTE NASAibiblio

    NASA TECHNICAL NOTE NASA TN D-7289 OI 00 N h APOLLO EXPERIENCE REPORTGUIDANCE AND CONTROL SYSTEMS Digital Autopilot Design Development by Willium H. Peters und Kenneth J. Cox Manned S ucecm Center Housto Texus 77058 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D. C. JUNE 1973

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  • NASATechnical Notes

    1869 Pomona Road Unit A. Corona CA 92880. . aeroinstruments sbcglobal. (Aerophysics acquired much of the intellectual property from Task/Able) Triumph Aerospace Force Measurement Systems. AIAA Recommended Practice for Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (R) AIAA

    Get Price
  • NASADryden Technical Report Server

    Report Number NASA-TN-D-6800. Performing Organization NASA Dryden Flight Research Center Edwards CA. Availability Format (s) on-line PDF (12 838 KBytes) Report Date June 1972. No. Pages 371. FLIGHT-DETERMINED CHARACTERISTICS OF AN AIR INTAKE SYSTEM ON AN F-111A AIRPLANE Technical Note.

    Get Price
  • NACA TN-2662 MAY1952 NATIONAL ADVISORY COMMITTEE NOTE A

    NACA-TN-2662 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS TECHNICAL NOTE 2662A SUMMARY OF DIAGONAL TENSION PART IIEXPERIMENTAL EVIDENCE (MAY-1952) (KUHN P. PETERSON J.P. LEVIN L.). Methods of analyzing web systems working in diagonal tension have been given in Part I (NACA-TN-2661) of this paper.

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  • Technical NotesNASA

    Technical Notes Applies to Unified Submittal Descriptions All versions of SpecsIntact Previously there were nineteen Submittal types with NASA and Army utilizing ten submittal descriptions (SDs) and Navy using seventeen. To further standardize the technical content of specifications the three agencies agreed to implement a new Unified

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  • NASA TECHNICAL NOTE NASA TN D-6575

    nasa technical note nasa tn d-6575 ln h m 4 a summary of spin technology as related to light i general-aviation airplanes i by james s. bowman jre langley research center hampton va 23365 i national aeronautics and space administration washington d. c. december 1971

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  • NASA TECHNICAL NOTE NASA TN 0-6739

    NASA TECHNICAL NOTE APOLLO EXPERIENCE REPORTVOICE COMMUNICATIONS TECHNIQUES AND PERFORMANCE by John H. Dabbs and Oron L. Schmidt Manned Spacecraft Center Houston Texas 77058 NASA TN 0-6739 NA TlONAl AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON D. C. • MARCH 1972

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  • NASA TECHNICAL NOTE NASA TN D-6563

    NASA TN D- 5744 c. L tpt.51 NASA TECHNICAL NOTE NASA TN D-6563 DESIGN STUDY OF SHAFT FACE SEAL WITH SELF-ACTING LIFT AUGMENTATION VPerformance in Simulated Gas Turbine Engine Operation by Lawrence P. Lzldwig und Robert L. Johnson Lewis Reseurch Cepzter

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  • NASA TECHNICAL NOTE NASAibiblio

    NASA TECHNICAL NOTE NASA TN D-7289 OI 00 N h APOLLO EXPERIENCE REPORTGUIDANCE AND CONTROL SYSTEMS Digital Autopilot Design Development by Willium H. Peters und Kenneth J. Cox Manned S ucecm Center Housto Texus 77058 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D. C. JUNE 1973

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