For Internal Use Only

Total Page:16

File Type:pdf, Size:1020Kb

For Internal Use Only ENGINEERING LABORATORY MONTHLY PROGRESS REPORT FOR PERKJD DECEMBER 1, -1967 THROUGH DECEMBER 31, 1967 FOR INTERNAL USE-. ONLY NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MSFC - Form 1262 (Rev October 19-67) PROPULSION AND VEHICLE ENGINEERING LABORATORY MONTHLY PROGRESS REPORT (December 1, 1967 Through December 31, 1967) Materials Division Structures Division Vehicle Systems Division Advanced Studies Office Propulsion Division GEORGE C. MARSHALL SPACE FLIGHT CENTER TABLE OF CONTENTS Page 1. MATERIALS DIVISION .............................. 1 Saturn V ..................................... 1 I . S-IC Stage ................................ 1 A . Evaluation of Commercial Adhesives ........... 1 1 . Polyurethane Adhesives ................ 1 a . Aging Studies .................... 1 b . Additive and Primer Studies .......... 2 2. Silicone Adhesives .................... 2 B . Development and Evaluation of Potting Compounds and Conformal Coatings ................... 2 1. Development of Epoxys iloxane Embedment Materials .......................... 2 2 . Development of Conformal Coating Materials . 3 3 . Ceramic Potting Compounds ............. 4 C . Investigation of Spring Failure in the S-IC Stage LOX Prevalve .......................... 4 D . Stress Corrosion Studies of 17-7 PH Actuator Springs .............................. 4 I1 . Contract Research ........................... 4 A . Polymer Research. Development. and Testing .... 4 B . Development of Cryogenic and High Temperature Insulation Material ....................... 4 C . Analytical Methods Development .............. 5 D . Assessment and Evaluation of Blast Hazards ..... 5 E . Nondestructive Testing Techniques ............ 5 I11 . S-I1 Stage ................................. 5 A . Investigation of Failure of S-I1 Stage Interstage Fasteners ............................ 5 B . Evaluation of Foams for Applicability as S-I1 Stage Liquid Hydrogen Tank Insulation .......... 5 C . Inspection of the S-11-F /D Liquid Hydrogen Tank ... 6 D. Investigation of Cracking of 2014-T651 in S-I1 Stage Components .................... 6 E . Evaluation of Bolts for Use in the S-I1 Stage Thrust Stage Attachment ................... 6 F . Investigation of Repair Used on the S-I1 Stage Thor Test Tank ......................... 7 G . Developmental Welding .................... 7 H. Development of Standard Nondestructive Techniques for Inspection of Inert Gas Welds in the S-I1 Stage . 7 TABLE OF CONTENTS (Continued) Page I . Investigation of Nondestructive Techniques for Composite Materials .................. J . Investigation of Dye Penetrants for Use in Inspection of S-I1 Stage Hardware .......... K . S-I1 Stage. Project Management. Materials ..... 1. Pulsed Arc MIG Welding (PAMIG) ......... 2 . Liquid Hydrogen Tank Stress Relief Areas ... 3 . Spray Foam Insulation ................ IV . S-IVB Stage .............................. A . Study of Materials Problems Attendant to the S-IVB Workshop Program ................. 1. Study of Flammability of Materials ........ 2 . Study of the Outgassing Characteristics of Orbital Workshop Materials ........... B . S-IVB Stage. Project Management. Materials .... 1. Stress Corrosionof Belleville Springs ...... 2. Stress Corrosion of Thrust Vector Control System Parts ...................... 3 . Evaluation of MD-19 Thermal Control Coating . 4. Penetration Sealing Devices ............. 5 . Thermal Curtain Materials ............. 6 . Quick Opening Hatch Material ........... V . F- 1 Engine ............................... F- 1 Engine. Project Management. Materials .... VI . J-2Engine ............................... J-2 Engine. Project Management. Materials .... VII . Instrument Unit ............................ Study of Possible Gas Evolution in the Environmental Control System .............. VIII . Apollo Telescope Mount (ATM) .................. A . Investigation of Contamination and Contamination Sources ............................. B . Evaluation of Direct Current Motors for Use onATM ............................. C . InvestigationofATMBearingLubrication ...... D . Investigation of Thermal Control Materials forATM ............................. TABLE OF CONTENTS (Continued) Page IX . Nuclear Vehicle Technology ..................... 18 A. Investigation of Propellant Heating ............ 18 B . RIFT Tank Tests ........................ 19 C . Activation Analyses ...................... 19 Advanced Research and Technology ................... 20 I . Contract Research ........................... 20 A. Polymer Development and Characterization ...... 20 B . Adhesive Development .................... 20 C . Developmental Welding .................... 20 D. Thermal Control Coatings .................. 20 E . Physical and Mechanical Metallurgy ........... 20 F . Composite Material Development and Testing ..... 20 G . Lubricants and Lubricity ................... 20 H. CorrosioninAluminumandSteel ............. 20 I . Explosion Hazards and Sensitivity of Fuels ...... 21 J . Synergistic Effects of Nuclear Radiation. Vacuum. and Temperature on Materials ........ 21 K . Instrument Development ................... 21 I1 . General--I n-House ........................... 21 A . Development of High Temperature Resistant Polymers ............................. 21 B . Development and Characterization of Phospho- nitrilic Polymers ....................... 22 C . Development of Fluorinated Adhesives .......... 23 D. Development of Sealant Materials ............. 24 E . Development and Evaluation of Metallic Composites ............................ 24 F . Investigation of Stress Corrosion Characteristics of Various Alloys ....................... 25 G . Investigation of Stress Corrosion Induced Property Changes in Metals ................. 26 H. Analysis of Retro Rocket Exhaust ............. 27 I . Development and Evaluation of Materials for Electrical Contacts in Vacuum ............ 27 J . Development of Low Density Ceramic Foam ...... 28 K . Evaluation of Alloys ...................... 29 L . Developmental Welding .................... 29 M . Investigation of Electroplating Procedures ....... 30 N. Documentation Review ..................... 30 0 . Literaturesurvey ....................... 31 TABLE OF CONTENTS (Continued) Page Monthly Production Report ........................ 32 I . Radiography ............................... 32 I1 . Photography ............................... 32 I11 . Metallurgical and Metallographic Testing and Evaluation. 32 IV . SpectrographicAnalyses ....................... 33 V . Infrared Analyses ........................... 33 VI . Chemical Analyses ........................... 33 VII . Rubber and Plastics .......................... 34 VIII . Electroplating and Surface Treatment .............. 34 IX . Development Shop Production ................... 34 A . Manhours. Direct Labor ................... 34 B . Manhours . Nonroutine .................... 34 1. Saturn V Sled Test Module ............... 34 2 . Models of ATM Experiment Package ........ 34 3 . X-ray Astronomy Assembly Modification ..... 34 4 . GOX Impact Compression Tester .......... 34 5 . Flange Assembly NGTM ................ 34 6 . Bearing Test Assembly ................. 34 7 . ATM Mock-up Components .............. 35 8 . Water Cooling Manifold ................. 35 X. Miscellaneous .............................. 35 XI . Publications ............................... 35 2 . STRUCTURESDIVISION ............................. 37 Saturn IB ....................................... 37 S-IVB Stage ................................... 37 Control Relay Assembly ....................... 37 Saturn V .................................... .. 37 I . S-I1 Stage ................................. 37 A . Interstage Recirculation and 207 Container Battery Environment ..................... 37 B . Acoustic Testing of Forward Skirt ............ 38 C . S-I1 Weld Land Tests ..................... 38 D . S-I1 Lightweight Structural Test Program ....... 38 1. V7-21 ("A" Structure) ................. 38 2 . V7-22 (I1B" Structure) ................. 39 3 . V7-23 ("C" Structure) ................. 39 11 . S-IVB Stage ................................ 39 Acoustic Testing ........................ 39 I11 . Saturn V System ............................ 39 A . AS-502 Pull Test ........................ 39 B . Weld Evaluation Program .................. 40 TABLE OF CONTENTS (Continued) Page Apollo Application Program ........................... I . Apollo Telescope Mount ....................... A . Rack ................................ B . ATM Rack and ATM Shear Webs .............. I1 . Multiple Docking Adapter ...................... MDA Docking Ports ...................... I11 . Meteoroid Protection ......................... IV . MSFC Flight Experiment # 8 .................... 3 . VEHICLE SYSTEMS DIVISION ......................... SaturnIB ....................................... I . S-IVB Stage ............................... Pneumatic Consoles ...................... I1. General .................................. A . Composite Mechanical Schematics ............ B . Hazardous Gas Analyzer (HGA)............... C . Weight Status Reports ..................... D . Engineering Criteria and Specifications ......... SaturnV ........................................ I . S-IC Stage ................................ A . Propellant Dispersion System (PDS) ........... B . S-IC Hydraulic Supply and Checkout Unit (HSCU) ... C . Ground Hydraulic Accumulator Bank (GHAB) ..... D . Pneumatic Consoles ...................... E . Umbilicals ............................ I1. S-I1 Stage ................................
Recommended publications
  • Saturn V Data and Launch History Resized
    Saturn V 50th Anniversary Commemorative Evening, November 8, 1967. AS-501 / Apollo 4, Pad 39A, KSC, FL. The Saturn V Launch Vehicle With a capacity to boost a payload of 260,000 lb. into low Earth orbit, or a 100,000 lb. payload into a lunar trajectory, the Saturn V remains the most powerful launch vehicle yet to leave the Earth's atmosphere. It was capable of placing in orbit a payload more than four times heavier than the future Space Shuttle could lift, and was six times more powerful than the next largest expendable rocket of its day. The Saturn V was designed by NASA engineers at the Marshall Space Flight Center, (MSFC), in Huntsville, AL, under the direction of Dr. Wernher von Braun. Development began in January, 1962. A total of fifteen vehicles were produced. Thirteen flew missions. Characteristics Overall length: 281 ft. (booster), 363 ft. (with spacecraft). Maximum diameter: 33.0 ft. Weight at liftoff: 6,423,000 lbs. Trans-lunar payload capability approximately 107,350 lbs. Earth orbit payload capability, (two stage configuration); 212,000 lbs. Stages First Stage, (S-IC); Contractor: Boeing Assembled: New Orleans, LA . Length: 138 ft. Diameter: 33 ft. Weight: 5,022,674 lbs. fueled / 288,750 lbs. dry. Engines: F-1 (x5) Designed and manufactured by Rocketdyne, Canoga Park, CA. Propellants: LOX (Liquid Oxygen) / RP-1 (Kerosene.) Thrust: 7,610,000 lbs. During the production run, the F-1 was redesigned and up-rated in preparation for the later "J Series" of extended lunar missions. These missions carried heavier payloads. With up-rated engines, the S-IC produced 7,724,000 lbs.
    [Show full text]
  • SD 68-654-2 ENGINEERING COURSE for SATURN S-11 STAGE SYSTEMS for NASA and HEROICRELICS.ORG VOLUME 2 S-11 STAGE PROPULSION and MECHANICAL SYSTEMS November 1968
    SD 68-654-2 ENGINEERING COURSE FOR SATURN S-11 STAGE SYSTEMS FOR NASA AND HEROICRELICS.ORG VOLUME 2 S-11 STAGE PROPULSION AND MECHANICAL SYSTEMS November 1968 Approved by ~ B . Botfeld Manager, Mechanical Systems Analysis and Requirements S-II Engineering SPACE DIVISION NORTH AMERICAN ROCKWELL CORPORATION SD 68-654-2 ENGINEERING COURSE FOR SATURN S-11 STAGE SYSTEMS FOR NASA VOLUME 2 S-11 STAGE PROPULSION AND MECHANICAL SYSTEMS November 1968 Approved by :r B. Botfeld Manager, Mechanical Systems Analysis and Requirements S -II Engineering SPACE DIVISION NORTH AMERICAN ROCKWELL CORPORATION SPACE DIVISION oF HEROICRELICS.ORG THIS PAGE I NTENTIONALLY LEFT BLANK - ii - SD 68-654-2 SPACE DIVISION oF NORTH AMERICAN ROCKWELL CORPORATION FOREWORD This volume is one of four volumes comprised by the Engineering Course on Saturn S-II Systems f or NASA (SD 67-654) and is to be used only in conjunc­ tio n w ith the classroom presentation. The cour se is being presented in accordance with Change Order 1085 to Contract NAS7-200 . - 111 - SD 68-654-2 SPACE DIVISION oF HEROICRELICS.ORG THIS PAGE I NTENTIONALLY LEFT BLANK - iv- SD 68-654-2 SPACE DIVISION oF NORTH AMERICAN ROCKWELL CORPORAT ION CONTENTS Section Pag e S-11 STAGE PROPULSIO N SYS TEM 1 ENGINE SYSTEMS 1 Function 1 Engine System Features 1 Arrangement 1 Engine System Operating Features 4 Engine System Support Features. 9 Engine System Condition at Liftoff 11 MSC Console Displ ay 11 Engine System Flig ht Sequence 11 Major Engine Variation . 15 Engine System Performance and Requirements 15 ULLAGE MOTOR SYSTEM.
    [Show full text]
  • Apollo 17 Press
    7A-/ a NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Washington. D . C . 20546 202-755-8370 FOR RELEASE: Sunday t RELEASE NO: 72-220K November 26. 1972 B PROJECT: APOLLO 17 (To be launched no P earlier than Dec . 6) R E contents 1-5 6-13 U APOLLC 17 MISSION OBJECTIVES .............14 LAUNCH OPERATIONS .................. 15-17 COUNTDOWN ....................... 18-21 Launch Windows .................. 20 3 Ground Elapsed Time Update ............ 20-21 LAUNCH AND MISSION PROFILE .............. 22-32 Launch Events .................. 24-26 Mission Events .................. 26-28 EVA Mission Events ................ 29-32 APOLLO 17 LANDING SITE ................ 33-36 LUNAR SURFACE SCIENCE ................ 37-55 S-IVB Lunar Impact ................ 37 ALSEP ...................... 37 K SNAP-27 ..................... 38-39 Heat Flow Experiment ............... 40 Lunar Ejecta and Meteorites ........... 41 Lunar Seismic Profiling ............. 41-42 I Lunar Atmospheric Composition Experiment ..... 43 Lunar Surface Gravimeter ............. 43-44 Traverse Gravimeter ............... 44-45 Surface Electrical Properties 45 I-) .......... T Lunar Neutron Probe ............... 46 1 Soil Mechanics .................. 46-47 Lunar Geology Investigation ........... 48-51 Lunar Geology Hand Tools ............. 52-54 Long Term Surface Exposure Experiment ...... 54-55 -more- November 14. 1972 i2 LUNAR ORBITAL SCIENCE ............... .5 6.61 Lunar Sounder ................. .5 6.57 Infrared Scanning Radiometer ......... .5 7.58 Far-Ultraviolet Spectrometer ..........5
    [Show full text]
  • ULXISG LAZSLXXY PROP-LSZON and VEHICLZ EKG--YT' Prepared by Industrial Resources Grou?
    ACTIVE Z3XTFr1CTS ::ST PROP-LSZON AND VEHICLZ EKG--YT',A ULXISG LAZSLXXY Prepared by Industrial Resources Grou? Resources Yunagement Office AiResearch Yanuf acturing MS8-;'1%2i Development and Hanufacture of Trotective Clothing for Use in Hazardous Environments Brown Engineering Company Design, Development, Fabrication, and Delivery of Saturn V Tinstrument Unit Umbilical Connector Assemblies Brown Engineering Cornpany DesLgn, Development, Documentation, Fabrication, and Testing of Saturn V Simulator Instrument Unit Disconnect Carrier Assembly Kits 3rown Engineering Company ViSration Testing of Saturn ,nstrument-- Unit Hounting Con?onents Brown Engineering Company Verification of Criticality Data Denison Ecgineering Div. Qnaiification Test Program for -7. American Brake Shoe CO. high Pressure lump Used in the S-IC Ground Hydraulic Supply & C'neckout Douglas Aircraft Company Suman Engineering Design Criteria Study - - Greer Kydraulics, Inc. yhL ~s~-',i673 -0 S?are Parts ror ,ogistic~l ~~;~pi~~y~S~pport of S-IC Hydraulic Support and Checkout Units Greer Eiydraulics, Inc. iSAS8-54-74 Czsign, Devclop:~$znt, iilznuf aczuring, aild Delivery of Five Ground Support Hydraulic Systems and Checkout Units Idalter Edde and Co., Inc. XAS8-,1550 Ceslgn, 3~5:-ica:5on, Testing, an? Delivery o; . ive Xach S-IC Inert ??refill Unrts Walter Ridde and Co., Inc, i\;:S8-+;357 Feslgn, -Usvelopment, FabrlcaEion, Assembly, and Testin-tJ of a Truck-Mounted Flush and ?urge Ground Sup?ort Servicing System Hayes International Corp. Air Bearing Supply Distribucion and Konitoring System Hayes International Corp. Design, Develop, Fabricate, Test, and Delivery of Two Mobile Service Truck Units (M-1 and Sodiun Nitrite) - Jet Research Cezter, Inc. %S8-li484 im?act of S2nsltlvlzy of COITLETE Various Typzs and Sizes of Linear Shaped Charges Yfrtin-Marietta Corp.
    [Show full text]
  • SATURN I B LIQUID HYDROGEN ORBITAL Experl MENT Defl
    , NASA TECHNICAL NASA XbLX-53158 MEMORANDUM : NoT~M~..!1. 1964 SATURN IB LIQUID HYDROGEN ORBITAL EXPERlMENT DEFlNlTlON . by ADVANCED STUDIES OFFICE Propulsion and Vehicle Engineering Laboratory OTS PRICE XEROX NASA M ICRO FI LM George C. Marshall S’uce Fght Center, Hmtsuille, Alabama TECHNICAL MEMORANDUM X-53158 SATURN IB LIQUID HYDROGEN ORBITAL EXPERIMENT DEFINITION I' Compiled By Advanced Studies Office George C. Marshall Space Flight Center Huntsville , Alabama ABSTRACT A Liquid Hydrogen Orbital Experiment is defined, using Saturn IB iaunch vehicle SA-203, which will demonstrate the adequacy of the S-IVB/V continuous vent and propellant settling system prior to a Saturn V launch. The state -of-the -art knowledge of cryogenic propellant behaviour under weightless environment will be significantly advanced by this observation of transient effects on liquid hydrogen through two television cameras mounted on the manhole cover of the S-IVB stage LH2 tank. The experiment justification, objectives, and S-IVB stage instrumentation are presented in detail. The liquid hydrogen experiment was proposed and defined by the Propulsion Division of Propulsion and Vehicle Engineering Laboratory. This report was compiled for R&D Operations with the assistance of Aero -A str odynamic s Labor a tory, Astfionic s Labor ator y, and Quality and Reliability Assurance Laboratory and complements NASA TM X-53 159, "Saturn IB Liquid Hydrogen Experiment Preliminary Lau Design Definition. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION AXO.LVXOBV? 3NIl333NI3N3 313IH3A aNV NOISTndOXd X3LN33 LH3ITJ 33VdS T?VHS~~'333XO33-VSVN TABLE OF CONTENTS Page SUMMARY .................................... 1 SE C TION I. INTRODUCTION ....................... 3 A. GENERAL .............................. 3 B. CONTINUOUS VENT AND LIQUID SETTLING .....
    [Show full text]
  • Space Security 2010
    SPACE SECURITY 2010 spacesecurity.org SPACE 2010SECURITY SPACESECURITY.ORG iii Library and Archives Canada Cataloguing in Publications Data Space Security 2010 ISBN : 978-1-895722-78-9 © 2010 SPACESECURITY.ORG Edited by Cesar Jaramillo Design and layout: Creative Services, University of Waterloo, Waterloo, Ontario, Canada Cover image: Artist rendition of the February 2009 satellite collision between Cosmos 2251 and Iridium 33. Artwork courtesy of Phil Smith. Printed in Canada Printer: Pandora Press, Kitchener, Ontario First published August 2010 Please direct inquires to: Cesar Jaramillo Project Ploughshares 57 Erb Street West Waterloo, Ontario N2L 6C2 Canada Telephone: 519-888-6541, ext. 708 Fax: 519-888-0018 Email: [email protected] iv Governance Group Cesar Jaramillo Managing Editor, Project Ploughshares Phillip Baines Department of Foreign Affairs and International Trade, Canada Dr. Ram Jakhu Institute of Air and Space Law, McGill University John Siebert Project Ploughshares Dr. Jennifer Simons The Simons Foundation Dr. Ray Williamson Secure World Foundation Advisory Board Hon. Philip E. Coyle III Center for Defense Information Richard DalBello Intelsat General Corporation Theresa Hitchens United Nations Institute for Disarmament Research Dr. John Logsdon The George Washington University (Prof. emeritus) Dr. Lucy Stojak HEC Montréal/International Space University v Table of Contents TABLE OF CONTENTS PAGE 1 Acronyms PAGE 7 Introduction PAGE 11 Acknowledgements PAGE 13 Executive Summary PAGE 29 Chapter 1 – The Space Environment:
    [Show full text]
  • Flight E'jaluation Kefqrt
    https://ntrs.nasa.gov/search.jsp?R=19700026640 2020-03-11T23:35:54+00:00Z SATURN S-IVB-501 STAGE FLIGHT E'JALUATION KEFQRT APRIL 1986 Dol,*L;L'AsQ- '-' MISS, LB b SPACE rqf5iFA4S D/WS/DN SATURN S-IVB-501 STAGE FLIGHT EVALUATION REPORT VOLUME I DOLJGLAS REPORT Skl-C7004 /iPHIL 1968 ) PREPARED 9 . SAlURN S-IVB TEST PLANLJIVG AND EVALIJATIOh C0MM.T; EE AND COORDINATED BY: .!. A. 'TOPIAS PFiOJEC- OFFlCc - Fl-nGHT TEST SA . JRN DELELOQME%TELJG.NEER!NG F REPARED FOR: N;T!ONAL ESONAUTICS AND ISPACE ADMINIST ~ATl0.r UNDER NASA CONTRACT NAC7-10' PIRECTOR, HUNTIt'5TON EACH DEVF-OPMENT, ILNGINZERING - SATURN/APOLI 3 PROGRAM QOI'GLRS M/SS/LE 6; SPACE L1"Ya!TEMSf7/V/S/(=IA/ SPArE SYSTEMS CENTER - HUNT IN~TONBEAC);, CC LlFORNlA SATURN AS-5i11 VEH' ,LE LIFTOFF ABSTRACT This report, prepared in two volumes, presents the evaluation results of the preiaunch coi*7tdown, powered flight, and orbital ~haseo' the S-IVB-501 stage which was launched on 9 November 1967 as the third stage of the Saturn AS-501 vehicle. Volume I contains the first 15 sections of the report; Volume I1 contains the remaining 10 sections and 6 appendixes of the report. All flight objectives were satisfied and the stage and ground support equipnent functioned as anticipated. The report is a contractual document as outlined in NASA Report PISFC-DRL-021, Contract Data Requirements, Saturn S-IVB Stage and GSE, dated 1 February 1968, Revision A. I*Lwas prepared by the Saturn S-IVR Test Planning and Evaluation Committee and coordinated by the Saturn S-IVB Project Office of the Douglas Aircraft Company, Missile and Space Systems Division.
    [Show full text]
  • Apollo 15 Press
    '/ .74 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WO 2-4155 NEWS WASHINGTON,D .C. 20546 TELS' WO 3-6525 FOR RELEASE: THURSDAY A.M. July 15, 1971 RELEASE NO: 71-119K PROJECT: APOLLO 15 (To be launched no P earlier than July 26) R E contents S S K I T -i2- -more- -i3- -0- 4 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (m2) 962-4155 N E W S WASHINGT0N.D.C. 20546 ~LS: (2132) 963-6925 Ken AtChison/Howard Allaway FOR RELEASE: THURSDAY, A.M. (Phone 202/962-0666) July 15, 1971 RELEASE NO: 71-119 APOLLO 15 LAUNCH JULY 26 The 12-day Apollo 15 mission, scheduled for launch on July 26 to carry out the fourth United States manned eyplora- tion of the Moon, will: - Double the time and extend tenfold the range of lunar surface exploration as compared with earlier missions; - Deploy the third in a network of automatic scientific stations; - Conduct a new group of experiments in lunar orbit; and - Return to Earth a variety of lunar rock and soil samples. Scientists expect the results will greatly increase man's knowledge both of the Moon's history and composition and of the evolution and dynamic interaction of the Sun-Earth system. This is so because the dry, airless, lifeless Moon still bears records of solar radiation and the early years of solar system history that have been erased from Earth. Observations of current lunar events also may increase understanding of similar processes on Earth, such as earthquakes. -more- 6/30/71 b . -2- The Apoll 15 lunar module will mak its descent over the Apennine peaks, one of the highest mountain ranges on the Moon, to land near the rim of the canyon-like Hadley Rille.
    [Show full text]
  • For Internal Use Only
    PROPULSION AND VE MCLE MONTWLY PROGRESS REPORT For Period March 1, 1967, Through March 3 1, 1967 FOR INTERNAL USE ONLY GEORGE C. #ff#TsV!IfE. ALABAMA NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MSFC - Fmm 1262 (September 1961) PROPULSION AND VEHICLE ENGINEERING LABORATORY MONTHLY PROGRESS REPORT (March 1, 1967, Through March 31, 1967) Materials Division Vehicle Systems Division Advanced Studies Office Propulsion Division Structures Division GEORGE C. MARSHALL SPACE FLIGHT CENTER TABLE OF CONTENTS Page MATERIALS DIVISION . 1 Saturn IB . 1 I. S-IB Stage. 1 A. Evaluation of Aging Treatment for 7075-T6 Aluminum Components in Reducing Susceptibility to Stress Corrosion ..................... 1 B. Corrosion Effects of MIL-H-5606 Hydraulic Oil. 1 11. H-1 Engine . 1 Investigation of Cause of Leakage in an H- 1 Engine Turbine Manifold . 1 Saturn V. .. 2 I. 5-IC Stage . 2 A. Investigation of the Failure of a Component of an S-IC Hold-down Arm . 2 B. Evaluation of Commercial Adhesives . 2 1. Investigation of Polyurethane Adhesives ................. 2 a. Study of Environmental Effects on Strength of Polyurethane Adhesives . 2 b. Reevaluation ofNarmco7343/ 7 139 Cure Cycle. 2 c. Evaluation of Curalon- L as C 1.1rative for DuPonts ' Adiprene L-100 and L-315. 3 2. Investigation of Surface Preparation for Bonding Stainless Steel Adherends 3 3. Investigation of Semi-organic Structural Adhesives. 3 C. Development and Evaluation of Potting Compounds and Conformal Coatings. 4 1. Development of Epoxy-Siloxane Embedment Materials . 4 2. Implementation of Molc:ct~lar Distillation Apparatils . 5 3. Development of Conformal Coating Materials . 5 TAB LE OF CONTENTS {Continued) Page D, Nondestructive Examination of Fuel Valve Castings.
    [Show full text]
  • NASA) Employed Foreign Scientists and Engineers to Work in Various Positions
    The National Archives At Atlanta Description of Records of the National Aeronautics and Space Administration Research Room Hours: 8:30 a.m. – 5:00 p.m. Tuesday – Saturday National Archives at Atlanta 5780 Jonesboro Rd. Morrow, GA 30260 National Advisory Committee for Aeronautics (Predecessor) Special Program Files Regarding Weather ............................................................................................................... 4 George C. Marshall Space Flight Center Administration Program and Support, ..................................................................................................................... 4 Administrative Services Division ................................................................................................................................ 5 Advanced System Office.............................................................................................................................................. 5 Astrionics Laboratory ................................................................................................................................................. 5 Astronautics Laboratory ............................................................................................................................................. 6 Central System Engineering ....................................................................................................................................... 6 Engine Program Office ..............................................................................................................................................
    [Show full text]
  • NASA Connectionto Aerospace
    STI CENTER -GS 53-45/100 NASA JOHNSON SPACE CEN'TER HOUSTON, TX 77058-3696 NASA Connectionto Aerospace A Service of: NationalAeronautiCSand Space Adrrdnistration SCII_IqTIFIC TgCNNICAUb IN FORI¢IATION GEORGE C. MARSHALL SPACE FLIGHT CENTER MPR-SAT-FE6-9-7 SATURNV LAUNCHVEHICLE _ FLIGHT I'VALUATIONREPORT-AS-50_ ,,i ,APOLLO 10 MI SSION PREPAREDBY SATURNFLIGHTEVALUATIONWORKINGGROUP C_ & 0 r_ Z I c_ m I im m MPR-SAT-FE-69-7 SATURN V LAUNCH VEHICLE FLIGHT EVALUATION REPORT - AS-505 APOLLO I0 MISSION BY Saturn Flight Evaluation Working Group George C. Marshall Space Flight Center ABSTRACT Saturn V AS-505 (Apollo lO Mission) was launched at 12:49:00 Eastern Daylight Time on May 18, 1969, from Kennedy Space Center, Complex 39, Pad B. The vehicle lifted off on schedule on a launch azimuth of 90 degrees east of north and rolled to a fli.ght azimuth of 72.028 degrees east of north. The launch vehicle successfully placed the manned spacecraft in the planned translunar injection coast mode. The S-IVB/IU was placed in a solar orbit with a period of 344.9 days by a combination of continuous LH2 vent, the contingency experiment of propellant lead, a LOX dump and APS ullage burn. The Major Flight Objectiw_s and the Detailed Test Objectives of this mission were completely accomplished. No failures, anomalies, or de- viations occurred that seriously affected the flight or mission. Any questions or comments pertaining to the information contained in this report are invited arid should be directed to: Director, George C. Marshall Space Flight Center Huntsville_,
    [Show full text]
  • HISTORY of ON-ORBIT SATELLITE FRAGMENTATIONS 13Th Edition
    JSC 62530 HISTORY OF ON-ORBIT SATELLITE FRAGMENTATIONS 13th Edition Orbital Debris Program Office May 2004 National Aeronautics and Space Administration Lyndon B. Johnson Space Center Houston, TX 77058 HISTORY OF ON-ORBIT SATELLITE FRAGMENTATIONS 13th Edition May 2004 Prepared By: _________________________ David O. Whitlock Lockheed Martin Space Operations Approved By: _________________________ Jer-Chyi Liou, Ph.D. Lockheed Martin Space Operations Task Order Manager Approved By: _________________________ Nicholas L. Johnson NASA Johnson Space Center Chief Scientist and Program Manager Orbital Debris Program Office HISTORY OF ON-ORBIT SATELLITE FRAGMENTATIONS Thirteenth Edition (Information Cut-off Date: December 31, 2003) Nicholas L. Johnson David O. Whitlock Phillip Anz-Meador, Ph.D. M. Eleanor Cizek Sara A. Portman May 2004 Orbital Debris Program Office Johnson Space Center National Aeronautics and Space Administration JSC 62530 Preface to the Thirteenth Edition The first edition of the History of On-Orbit Satellite Fragmentations was published by Teledyne Brown Engineering (TBE) in August 1984, under the sponsorship of the NASA Johnson Space Center and with the cooperation of USAF Space Command and the US Army Ballistic Missile Command. The objective was to bring together information about the 75 satellites which had at that time experienced noticeable breakups. This update encompasses all known satellite fragmentations. This update is published by the NASA Johnson Space Center, Orbital Debris Program Office with support from Lockheed Martin Space Operations and Viking Science & Technology, Inc. Since the twelfth edition there have been 13 identified on-orbit breakups and five anomalous events. This activity has resulted in an approximately 7% increase in the historical cataloged debris count (since May 2001) which includes on-orbit and decayed objects, though less than 1% increase in the on-orbit debris count is observed.
    [Show full text]