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Progress Report on Apollo Program
PROGRESS REPORT ON APOLLO PROGRAM Michael Collins, LCol. USAF (M) Astronaut NASA-MANNED SPACECRAFT CENTER It is a great pleasure to be here today and to greet you hardy suMvors of the pool party. I will do my best to avoid loud noises and bright colors during my status report. Since the last SETP Symposium, the Apollo Program has been quite busy in a number of different areas. (Figure 1) My problem is to sift through this information and to talk only about those things of most interest to you. First, to review briefly our hardware, we are talking about two different spacecraft and two different boosters. (Figure 2) The Command Module is that part of the stack COLLINS which makes the complete round trip to the moon. Attached to it is the Service Module, containing expendables and a 20,000 pound thrust engine for maneuverability. The Lunar Module will be carried on later flights and is the landing vehicle and active rendezvous partner. The uprated Saturn I can put the Command and Service Modules into earth orbit; the Saturn V is required when the Lunar Module is added. Since the last symposium, we have flown the Command and Service Modules twice and the Lunar Module once, all unmanned. Apollo 4, the first Saturn V flight, was launched in November 1967. (Figure 3) The Saturn V did a beautiful, i.e. nominal, job of putting the spacecraft into earth parking orbit. After a coast period, the third stage (S-IVB by McDonnell Douglas) was ignited a second time, achieving a highly elliptical orbit. -
UAD Instance Chart 04.06.15 11:14
UAD Instance Chart 04.06.15 11:14 Search Site Hardware UAD-2 + Plug-Ins Store Blog Support About My.Uaudio Pressroom Contact Cart SUBSCRIBE TO THE Enter your email address Home > Support > UAD Support > UAD Compatibility > UAD Instance Chart UA NEWSLETTER UAD Instance Chart Online Support About This Chart The following table indicates DSP usage and instance counts for UAD Powered Plug-Ins. See bottom of page for more details about the chart. UAD Powered Plug-In DSP % SOLO DUO QUAD OCTO Contact Us Mono Stereo Mono Stereo Mono Stereo Mono Stereo Mono Stereo Phone Support 4K Buss Compressor 2.8% 3.4% 35 29 70 58 140 116 280 232 USA (toll free) 877-698-2834 4K Channel Strip * 7.4% 11.4% 17 11 34 22 68 44 136 88 International Ampex ATR-102 Mastering Tape Recorder 17.6% 29.0% 5 3 10 6 20 12 40 24 +1-831-440-1176 AMS RMX16 Digital Reverb 40.6% 41.1% 2 2 4 4 8 8 16 16 Germany, Austria, and Switzerland +31 (0) 20 800 4912 API 550A EQ 7.2% 11.7% 13 8 26 16 52 32 104 64 Fax +1-831-461-1550 API 560 EQ 9.2% 15.5% 10 6 20 12 40 24 80 48 Customer support is available from 9am to 5pm, Monday through Friday, PST API Vision Channel Strip * 22.4% 29.7% 4 3 8 6 16 12 32 24 Contact Support Bermuda Triangle 14.3% 28.4% 7 3 14 6 28 12 56 24 Submit a Request bx_digital V2 EQ & De-Esser 3.4% 4.9% N/A 20 N/A 40 N/A 80 N/A 160 Press, Review, and Advertising Inquiries Amanda Whiting bx_digital V2 Mono EQ & De-Esser 3.4% 3.8% 29 20 58 40 116 80 232 160 +1-831-440-1176 bx_refinement 12.3% 11.9% 7 7 14 14 28 28 56 56 Mailing Address Universal Audio, Inc. -
A Comparative Analysis of the Geology Tools Used During the Apollo Lunar Program and Their Suitability for Future Missions to the Om on Lindsay Kathleen Anderson
University of North Dakota UND Scholarly Commons Theses and Dissertations Theses, Dissertations, and Senior Projects January 2016 A Comparative Analysis Of The Geology Tools Used During The Apollo Lunar Program And Their Suitability For Future Missions To The oM on Lindsay Kathleen Anderson Follow this and additional works at: https://commons.und.edu/theses Recommended Citation Anderson, Lindsay Kathleen, "A Comparative Analysis Of The Geology Tools Used During The Apollo Lunar Program And Their Suitability For Future Missions To The oonM " (2016). Theses and Dissertations. 1860. https://commons.und.edu/theses/1860 This Thesis is brought to you for free and open access by the Theses, Dissertations, and Senior Projects at UND Scholarly Commons. It has been accepted for inclusion in Theses and Dissertations by an authorized administrator of UND Scholarly Commons. For more information, please contact [email protected]. A COMPARATIVE ANALYSIS OF THE GEOLOGY TOOLS USED DURING THE APOLLO LUNAR PROGRAM AND THEIR SUITABILITY FOR FUTURE MISSIONS TO THE MOON by Lindsay Kathleen Anderson Bachelor of Science, University of North Dakota, 2009 A Thesis Submitted to the Graduate Faculty of the University of North Dakota in partial fulfillment of the requirements for the degree of Master of Science Grand Forks, North Dakota May 2016 Copyright 2016 Lindsay Anderson ii iii PERMISSION Title A Comparative Analysis of the Geology Tools Used During the Apollo Lunar Program and Their Suitability for Future Missions to the Moon Department Space Studies Degree Master of Science In presenting this thesis in partial fulfillment of the requirements for a graduate degree from the University of North Dakota, I agree that the library of this University shall make it freely available for inspection. -
Why NASA Consistently Fails at Congress
W&M ScholarWorks Undergraduate Honors Theses Theses, Dissertations, & Master Projects 6-2013 The Wrong Right Stuff: Why NASA Consistently Fails at Congress Andrew Follett College of William and Mary Follow this and additional works at: https://scholarworks.wm.edu/honorstheses Part of the Political Science Commons Recommended Citation Follett, Andrew, "The Wrong Right Stuff: Why NASA Consistently Fails at Congress" (2013). Undergraduate Honors Theses. Paper 584. https://scholarworks.wm.edu/honorstheses/584 This Honors Thesis is brought to you for free and open access by the Theses, Dissertations, & Master Projects at W&M ScholarWorks. It has been accepted for inclusion in Undergraduate Honors Theses by an authorized administrator of W&M ScholarWorks. For more information, please contact [email protected]. The Wrong Right Stuff: Why NASA Consistently Fails at Congress A thesis submitted in partial fulfillment of the requirement for the degree of Bachelors of Arts in Government from The College of William and Mary by Andrew Follett Accepted for . John Gilmour, Director . Sophia Hart . Rowan Lockwood Williamsburg, VA May 3, 2013 1 Table of Contents: Acknowledgements 3 Part 1: Introduction and Background 4 Pre Soviet Collapse: Early American Failures in Space 13 Pre Soviet Collapse: The Successful Mercury, Gemini, and Apollo Programs 17 Pre Soviet Collapse: The Quasi-Successful Shuttle Program 22 Part 2: The Thin Years, Repeated Failure in NASA in the Post-Soviet Era 27 The Failure of the Space Exploration Initiative 28 The Failed Vision for Space Exploration 30 The Success of Unmanned Space Flight 32 Part 3: Why NASA Fails 37 Part 4: Putting this to the Test 87 Part 5: Changing the Method. -
Apollo 14 Press
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WO 2-4155 WASHINGT0N.D.C. 20546 lELS.wo 36925 RELEASE NO: 71-3K FOR RELEASE: THURSDAY A. M . January 21, 1971 P R E S S K I T -more - 1/11/71 2 -0- NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (m2) 962-4155 N E w s WASHINGTON,D.C. 20546 mu: (202) 963-6925 FOR RELEASE: THURSDAY A..M. January 21:, 1971 RELEASE NO: 71-3 APOLLO 14 LAUNCH JAN. 31 Apollo 14, the sixth United States manned flight to the Moon and fourth Apollo mission with an objective of landing men on the Moon, is scheduled for launch Jan. 31 at 3:23 p.m. EST from Kennedy Space Center, Fla. The Apollo 14 lunar module is to land in the hilly upland region north of the Fra Mauro crater for a stay of about 33 hours, during whick, the landing crew will leave the spacecraft twice to set up scientific experiments on the lunar surface and to continue geological explorations. The two earlier Apollo lunar landings were Apollo 11 at Tranquillity Base and Apollo 12 at Surveyor 3 crater in the Ocean of Storms. Apollo 14 prime crewmen are Spacecraft Commander Alan B. Shepard, Jr., Command Module Pilot Stuart A. Roosa, and Lunar Module Pilot Edgar I). Mitchell. Shepard is a Navy car-sain Roosa an Air Force major and Mitchell a Navy commander. -more- 1/8/71 -2- Lunar materials brought- back from the Fra Mauro formation are expected to yield information on the early history of the Moon, the Earth and the solar system--perhaps as long ago as five billion years. -
APOLLO EXPERIENCE REPORT - THERMAL PROTECTION SUBSYSTEM by Jumes E
NASA TECHNICAL NOTE NASA TN D-7564 w= ro VI h d z c Q rn 4 z t APOLLO EXPERIENCE REPORT - THERMAL PROTECTION SUBSYSTEM by Jumes E. Puulosky und Leslie G, St. Leger Ly12d012 B. Johlzson Space Center Honst0~2, Texus 77058 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, 0. C. JANUARY 1974 ~--_. - .. 1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. D-7564 4. Title and Subtitle 5. Report Date January 1974 APOLLOEXPERIENCEREPORT THERMAL PROTECTION SUBSYSTEM 6. Performing Organization Code I 7. Author(s) I 8. Performing Organization Report No. JSC S-383 James E. Pavlosky and Leslie G. St. Leger, JSC 10. Work Unit No. I 9. Performing Organization Name and Address 11. Contract or Grant No. Lyndon B. Johnson Space Center Houston, Texas 77058 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address 14. Sponsoring Agency Code National Aeronautics and SDace Administration Washington, D. C. 20546 1 15. Supplementary Notes The JSC Director waived the use of the International System of Units (SI) for this Apollo Experienc Report because, in his judgment, the use of SI units would impair the usefulness of th'e report or result in excessive cost. 16. Abstract The Apollo command module was the first manned spacecraft to be designed to enter the atmos- phere of the earth at lunar-return velocity, and the design of the thermal protection subsystem for the resulting entry environment presented a major technological challenge. Brief descrip- tions of the Apollo command module thermal design requirements and thermal protection con- figuration, and some highlights of the ground and flight testing used for design verification of the system are presented. -
Apollo 14 Lunar Landing Feb. 5
,$ VOLUME XIII NUMBER 8 February 4 National Aeronaulics and Sp :e Administration ,, Ames Research Center. Moffeft Field. California AmesMagnetometer on Apollo 14 The Apollo 14 astronauts will hours of operation. chart local magneticfields on the The devicewill be carriedon the surface of the moon, in the hilly outside of the Lunar Module near upland region of the Fra Mauro one of the landinglegs. It will be landing site, using a highly spe- transferredto the Mobile Equip- cialized,Ames designedand built, meat Transporter (MET) for mov- portablemagnetometer. ing on the surface of the moon. The astronautswill transport To use the instrument,one of the the lightweightmagnetometer on the astronautswill set up the sensor two-wheeledpush cart which car- head on the tripod and deploy it ries all the mission’sportable ex- about 40 feet from the electronics periments. package and indicators,which are Ames’ Dr. Palmer Dyal, Special left on the MET. He then calls ProjectsOffice, proposed the por- out readings from three meters on table magnetometerexperimentand the electronicspackage over the is the principalinvestigator for the voice communicationlink to Mission Apollo 14 experiment.Co-investi- ControlCenter at Houston.Then he gators on the experiment are Dr. rotates the cubical sensor head on FIRST AMERICAN TO JOURNEY INTO SPACE . Al.an B. Charles Sonett of Ames, Dr. Gene the tripodto an oppositeposition Shepard, Jr., is pictured as he was recovered following his Simmons of M.S.C. and Dr. Robert to fine tune the sensor and its suborbitalflight, the first in the Project Mercury program,on DuBois of the Universityof Okla- electronics.Be then calls out the May 5, t961. -
Apollo 14 Press
/ 17,° " 4 c 0 /r- NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WO 2-4155 FELS . WASHINGTON, D .0 . 20546 WO 3-6925 RELEASE NO: 71-3K FOR RELEASE:THURSDAY A.M. January 21, 1971 PROJECT: APOLLO 14 P (To be launched no earlier than Jan. 31) Eli?:4S7D7 5T- amuouAfX Ce4lift R FEB 1 ign contents E FPFITZcItt‘ GENERAL RELEASE 1-5 S COUNTDOWN 6 7 LAUNCH AND MISSION PROFILE 8 9 Launch Opportunities 9 Ground Elapsed Time Update 10 Launch Events 11 Mission Events 12-22 S Entry Events 23-24 RECOVERY OPERATIONS 25 Crew and Sample Return Schedule 26 MISSION OBJECTIVES 27 Lunar Surface Science 27-39 Lunar Orbital Science 39-46 Engineering/Operational Objectives 46-47 APOLLO LUNAR HAND TOOLS 48-51 FRA MAURO LANDING SITE 52-53 1‹: PHOTOGRAPHIC EQUIPMENT 54-55 TELEVISION 56 Apollo 14 TV Schedule 57-58 ZERO-GRAVITY INFLIGHT DEMONSTRATIONS 59 Electrophoretic Separation 59-61 Heat Flow and Convection 61 Liquid Transfer 62 Composite Casting 62-63 ASTRONAUTS AND CREW EQUIPMENT 64 Space Suits 64-69 Personal Hygiene 70 Medical Kit 70 Survival Kit 71 Crew Food 71 Prime Crew Biographies 72-78 Backup Crew Biographies 79-84 Flight Crew Health Stabilization Program 85 -more- 2 APOLLO 14 FLAGS, LUNAR MODULE PLAQUE 86 LUNAR RECEIVING LABORATORY (LRL) 87- 88 Sterilization and Release of Spacecraft 88-89 SATURN V LAUNCH VEHICLE 90 First Stage 90 Second Stage 90 Third Stage 90-91 Instrument Unit 92 Propulsion 92 Major Vehicle Changes 93 APOLLO SPACECRAFT 94-96 Command-Service Module Modifications 96-97 Lunar Module (LM) 98-100 MANNED -
Apollo 13 Mission Review
APOLLO 13 MISSION REVIEW HEAR& BEFORE THE COMMITTEE ON AERONAUTICAL AND SPACE SCIENCES UNITED STATES SENATE NINETY-FIRST CONGRESS SECOR’D SESSION JUR’E 30, 1970 Printed for the use of the Committee on Aeronautical and Space Sciences U.S. GOVERNMENT PRINTING OFFICE 47476 0 WASHINGTON : 1970 COMMITTEE ON AEROKAUTICAL AND SPACE SCIENCES CLINTON P. ANDERSON, New Mexico, Chairman RICHARD B. RUSSELL, Georgia MARGARET CHASE SMITH, Maine WARREN G. MAGNUSON, Washington CARL T. CURTIS, Nebraska STUART SYMINGTON, bfissouri MARK 0. HATFIELD, Oregon JOHN STENNIS, Mississippi BARRY GOLDWATER, Arizona STEPHEN M.YOUNG, Ohio WILLIAM B. SAXBE, Ohio THOJfAS J. DODD, Connecticut RALPH T. SMITH, Illinois HOWARD W. CANNON, Nevada SPESSARD L. HOLLAND, Florida J4MES J. GEHRIG,Stad Director EVERARDH. SMITH, Jr., Professional staffMember Dr. GLENP. WILSOS,Professional #tad Member CRAIGVOORHEES, Professional Staff Nember WILLIAMPARKER, Professional Staff Member SAMBOUCHARD, Assistant Chief Clerk DONALDH. BRESNAS,Research Assistant (11) CONTENTS Tuesday, June 30, 1970 : Page Opening statement by the chairman, Senator Clinton P. Anderson-__- 1 Review Board Findings, Determinations and Recommendations-----_ 2 Testimony of- Dr. Thomas 0. Paine, Administrator of NASA, accompanied by Edgar M. Cortright, Director, Langley Research Center and Chairman of the dpollo 13 Review Board ; Dr. Charles D. Har- rington, Chairman, Aerospace Safety Advisory Panel ; Dr. Dale D. Myers, Associate Administrator for Manned Space Flight, and Dr. Rocco A. Petrone, hpollo Director -___________ 21, 30 Edgar 11. Cortright, Chairman, hpollo 13 Review Board-------- 21,27 Dr. Dale D. Mvers. Associate Administrator for Manned SDace 68 69 105 109 LIST OF ILLUSTRATIOSS 1. Internal coinponents of oxygen tank So. 2 ---_____-_________________ 22 2. -
1 Reading Athenaios' Epigraphical Hymn to Apollo: Critical Edition And
Reading Athenaios’ Epigraphical Hymn to Apollo: Critical Edition and Commentaries DISSERTATION Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy in the Graduate School of The Ohio State University By Corey M. Hackworth Graduate Program in Greek and Latin The Ohio State University 2015 Dissertation Committee: Fritz Graf, Advisor Benjamin Acosta-Hughes Carolina López-Ruiz 1 Copyright by Corey M. Hackworth 2015 2 Abstract This dissertation is a study of the Epigraphical Hymn to Apollo that was found at Delphi in 1893, and since attributed to Athenaios. It is believed to have been performed as part of the Athenian Pythaïdes festival in the year 128/7 BCE. After a brief introduction to the hymn, I provide a survey and history of the most important editions of the text. I offer a new critical edition equipped with a detailed apparatus. This is followed by an extended epigraphical commentary which aims to describe the history of, and arguments for and and against, readings of the text as well as proposed supplements and restorations. The guiding principle of this edition is a conservative one—to indicate where there is uncertainty, and to avoid relying on other, similar, texts as a resource for textual restoration. A commentary follows, which traces word usage and history, in an attempt to explore how an audience might have responded to the various choices of vocabulary employed throughout the text. Emphasis is placed on Athenaios’ predilection to utilize new words, as well as words that are non-traditional for Apolline narrative. The commentary considers what role prior word usage (texts) may have played as intertexts, or sources of poetic resonance in the ears of an audience. -
Project: Apollo 8
v ._. I / I NATIONAL AERONAUTICS AND SPACE ADMINISTRATION TELS WO 2-4155 NEWS WASHINGTON,D.C.20546 • WO 3-6925 FOR RELEASE: SUNDAY December 15, 1968 RELEASE NO: 68.208 P PROJECT: APOLLO 8 R E contents GENERAL RELEASE----------~-------~·~-~-~--~~----~----~-~--~-l-lO MISSION OBJECTIVES------------------------------------------11 SEQUENCE OF EVENTS-------------~-------------~----~----~--~~12-14 5 Launch W1ndow~~-~----~--~-~--~-------~-----~---------w--~-14 MISSION DESCRIPTION-----------------------------------------15-19 FLIGHT PLAN--~---~-----·------------~------~----~---~----~--20-23 ALTERNATE MISSIONS---------------------------------~--------24-26 5 ABORT MODES-----~--------------~--~--~------------~---~~--~-27~29 PHOTOGRAPHIC TASKS------------------------------------------30-32 SPACECRAFT STRUCTURE SYSTEMS--------------------------------33-37 SATURN V LAUNCH VEHICLE-------------------------------------38-50 APOLLO 8 LAUNCH OPERATIONS----------------------------------51.64 MISSION CONTROL CENTER--------------------------------------65-66 MANNED SPACE FLIGHT NETWORK---------------------------------67-71 APOLLO 8 RECOVERY-------------------------------------------72-73 APOLLO 8 CREW-------------~--~--~~-~~---~---~~~-------------74-86 K LUNAR DESCRIPTION-------------------------------------------87-88 APOLLO PROGRAM MANAGEMENT/CONTRACTORS---~-------------------39-94 I APOLLO 8 GLOSSARY-------- -----------------------------------95-101 T -0- 12/6/68 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WO 2-4155 NEWS WASHINGTON, D.C. 20546 TELS. -
Appendix a Apollo 15: “The Problem We Brought Back from the Moon”
Appendix A Apollo 15: “The Problem We Brought Back From the Moon” Postal Covers Carried on Apollo 151 Among the best known collectables from the Apollo Era are the covers flown onboard the Apollo 15 mission in 1971, mainly because of what the mission’s Lunar Module Pilot, Jim Irwin, called “the problem we brought back from the Moon.” [1] The crew of Apollo 15 carried out one of the most complete scientific explorations of the Moon and accomplished several firsts, including the first lunar roving vehicle that was operated on the Moon to extend the range of exploration. Some 81 kilograms (180 pounds) of lunar surface samples were returned for anal- ysis, and a battery of very productive lunar surface and orbital experiments were conducted, including the first EVA in deep space. [2] Yet the Apollo 15 crew are best remembered for carrying envelopes to the Moon, and the mission is remem- bered for the “great postal caper.” [3] As noted in Chapter 7, Apollo 15 was not the first mission to carry covers. Dozens were carried on each flight from Apollo 11 onwards (see Table 1 for the complete list) and, as Apollo 15 Commander Dave Scott recalled in his book, the whole business had probably been building since Mercury, through Gemini and into Apollo. [4] People had a fascination with objects that had been carried into space, and that became more and more popular – and valuable – as the programs progressed. Right from the start of the Mercury program, each astronaut had been allowed to carry a certain number of personal items onboard, with NASA’s permission, in 1 A first version of this material was issued as Apollo 15 Cover Scandal in Orbit No.