Lecture 4 Page 1 Overview

Total Page:16

File Type:pdf, Size:1020Kb

Lecture 4 Page 1 Overview Exploring the Solar System Lecture 4: Exploration of the Moon Professor Paul Sellin Department of Physics University of Surrey Guildford UK Page 1 Paul Sellin Lecture 4 Page 1 Overview Exploration of the Moon: Moon probes: Luna, Ranger and Lunar Orbiter programmes Surveyor: the first controlled landing on the Moon Apollo: manned spaceflight to the Moon Samples from the Moon – lunar geology Page 2 Paul Sellin Lecture 4 Page 2 Exploration of the Moon Lunar missions covered the period 1959 to the 1990s: Luna 1, 2, 3 sent in 1959 by the Soviet Union to approach the Moon Project Ranger started in 1960 by the US, transmitting close-up views of the Moon’s surface before crashing into the Moon Lunar Orbiter programme: 5 spacecraft from 1966-1967 competed a high resolution photographic survey of the Moon’s surface, showing features as small as 1m. This data was used to select possible landing sights for the Apollo landings Surveyor programme: 5 unmanned spacecraft landed on the Moon during 1966-1968. Data from these spacecraft proved that the Moon’s surface was solid, and not a thick layer of dust Apollo consisted of 6 manned landings on the Moon – Apollo 11 in July 1969 followed by Apollo 14-17, landing in progressively more challenging terrain Unmanned Soviet spacecraft landed on the Moon from 1966 – 1976, with Luna 9 landing 4 months after the US Surveyor 1 in 1966. In the 1970s Luna spacecraft landed vehicles which explored the surface, and returned rock samples to Earth Clementine spent 2 months observing the Moon in 1994, carrying various UV/Vis/IR imaging cameras which revealed the atomic composition of large areas of the Moon’s surface Page 3 Paul Sellin Lecture 4 Page 3 Ranger programme The Ranger project of the 1960s was the first U.S. effort to launch probes directly toward the Moon. Ranger spacecraft were equipped with 6 TV cameras which transmitted close-up view of the Moon before they crash-landed into its surface. A variety of difficulties plagued the first several attempted missions in this series, but the Rangers 7-9 were a complete success Ranger 1: Launched 23 August 1961 Failed to leave Earth parking orbit Ranger 2: Launched 18 November 1961 Failed to leave Earth parking orbit Ranger 3: Launched 26 January 1962 Earth contact lost, missed the Moon by ~36,800 km Ranger 4: Launched 23 April 1962 Sequencer failed, impacted the Moon 26 April 1962 Ranger 5: Launched 18 October 1962 Earth contact lost, missed the Moon by 725 km Ranger 6: Launched 30 January 1964 Cameras failed, impacted the Moon 2 February 1964 Ranger 9 http://www.jpl.nasa.gov/missions/past/ranger.htmlPage 4 Paul Sellin Ranger 1 was launched from Cape Canaveral, Florida, on August 23, 1961, followed by the launch of Ranger 2 on November 18 of that year. In both cases, the Agena B rocket engine failed to restart and both spacecraft reentered Earth's atmosphere a short time later. Ranger 3 was launched January 26, 1962, but an inaccuracy put it off course and it missed the Moon. Ranger 4 had a perfect launch on April 23 of that year, but the spacecraft was completely disabled. The project team tracked the seismometer capsule to impact just out of sight on the far side of the Moon, validating the spacecraft's communications and navigation system. Ranger 5 missed the Moon following its launch on October 18, 1962, and was disabled. Ranger 6 was launched January 30, 1964, and had a flawless flight culminating in impact as planned on the Moon; its television system, however, was disabled by an in-flight accident and could take no pictures. The next three Rangers, with a redesigned television, were completely successful. Ranger 7 was launched July 28, 1964, and sent more than 4,300 pictures on its way down to target in a lunar plain, soon named Mare Cognitum, south of the crater Copernicus. Following launch on February 17, 1965, Ranger 8 successfully completed its mission with a planned crash-landing in Mare Tranquillitatis, where the Apollo 11 astronauts would land 4-1/2 years later. Ranger 8 garnered more than 7,300 images. Ranger 9 was launched March 21, 1965, and impacted the Moon in the 90- kilometer-diameter (75-mile) crater Alphonsus, sending back more than 5,800 images. Lecture 4 Page 4 Ranger images (1) The last two pictures taken by Ranger 9 before impact onto the lunar surface on the floor of Alphonsus crater. The top image was taken at a distance of 600m 0.25s before impact. The frame is about 70 m across. The lower frame includes most of the area on the left of the Ranger 9 view of crater Alphonsus upper image and was taken 3 minutes before impact, at a from 1.2km 4.5s prior to impact. distance of 442km The image is approximately 50 meters across. http://www.jpl.nasa.gov/missions/past/ranger.htmlPage 5 Paul Sellin Ranger 9 image of Alphonsus crater (diameter 108 km) from a distance of 442 km, taken about 3 minutes before impact in the upper right portion of the crater. At left is the northeastern edge of Mare Nubium. The crater adjacent to Alphonsus at the bottom is the 39 km diameter Alpetragius. Davy crater is at upper left. North is at 12:30. Ranger 9 impacted the Moon on 24 March 1965 at 14:08:20 UT. Lecture 4 Page 5 Ranger images (2) Ranger 9 image from 2500 km showing Ranger 9 image taken 54 seconds before impact, at Ptolemaeus, Alphonsus, and Albategnius 136km. The raised area at lower center is the central craters. peak of Alphonsus crater floor. Page 6 Paul Sellin (left) Ptolemaeus is the large (164 diameter) flat-floored crater at the top. Alphonsus, diameter 108 km, is at lower left and the 114 km Albategnius crater is at lower right. The terminator runs through the lower corner. Ranger 9 impacted in Alphonsus crater 18.5 minutes after this image was taken. North is at 12:30 (right) This image was taken from a distance of 136 km. The impact point of Ranger 9 is to the right of the central reticle, about 60% of the way from the central reticle to the edge of the frame. The image is 60 km across and north is at 12:30. Lecture 4 Page 6 Lunar Orbiter 5 Lunar Orbiters sent back a total of 2180 high resolution and 882 medium resolution images of the Moon’s surface, covering 99.5% of the Moon’s surface with resolution down to 1m. The micrometeoroid experiments recorded 22 impacts showing the average micrometeoroid flux near the Moon was about two orders of magnitude greater than in interplanetary space but slightly less than the near Earth environment. The radiation experiments confirmed that the design of Apollo hardware would protect the astronauts from average and greater-than-average short term exposure to solar particle events. Page 7 Paul Sellin http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=1967-075A Lunar Orbiter 5, the last of the Lunar Orbiter series, was designed to take additional Apollo and Surveyor landing site photography and to take broad survey images of unphotographed parts of the Moon's far side. It was also equipped to collect radiation intensity, and micrometeoroid impact data and was used to evaluate the Manned Space Flight Network tracking stations and Apollo Orbit Determination Program. The spacecraft was placed in a cislunar trajectory and on 5 August 1967 was injected into an elliptical near polar lunar orbit 194.5 km x 6023 km with an inclination of 85 degrees and a period of 8 hours 30 minutes. On 9 August the orbit was lowered to a 99 km x 1499 km, 3 hour 11 minute period. The photographic portion of the mission ended on 18 August. The spacecraft acquired photographic data from August 6 to 18, 1967, and readout occurred until August 27, 1967. A total of 633 high resolution and 211 medium resolution frames at resolution down to 2 meters were acquired, bringing the cumulative photographic coverage by the 5 Lunar Orbiters to 99% of the Moon's surface. Accurate data were acquired from all other experiments throughout the mission. The spacecraft was tracked until it impacted the lunar surface on command on January 31, 1968. The use of Lunar Orbiters for tracking to evaluate the Manned Space Flight Network tracking stations and Apollo Orbit Determination Program was successful, with three Lunar Orbiters (2, 3, and 5) being tracked simultaneously from August to October 1967. The Lunar Orbiters were all eventually commanded to crash on the Moon before their attitude control gas ran out so they would not present navigational or communications hazards to later Apollo flights. Lecture 4 Page 7 Marius crater Lunar Orbiter 5 image of the plateau west-northwest of Marius crater on the Moon. Note the two sinuous rilles which cut across a ridge at the center of the image. Also visible are volcanic domes and cones. The round "cobra-head" feature at the center left is roughly 2.5 km in diameter. The image is 80 km across and north is at 2:30 All Lunar Orbiter images from: http://nssdc.gsfc.nasa.gov/imgcat Page 8 Paul Sellin Lecture 4 Page 8 Aristarchus crater Lunar Orbiter 5 view of Aristarchus crater on the Moon. The crater is approximately 40 km in diameter, and 3.6 km in depth from rim to floor. Note the hummocky ejecta blanket surrounding the crater and the concentric and radial valleys along the crater walls, resulting from mass wasting.
Recommended publications
  • 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.
    [Show full text]
  • NASA's Lunar Atmosphere and Dust Environment Explorer (LADEE)
    Geophysical Research Abstracts Vol. 13, EGU2011-5107-2, 2011 EGU General Assembly 2011 © Author(s) 2011 NASA’s Lunar Atmosphere and Dust Environment Explorer (LADEE) Richard Elphic (1), Gregory Delory (1,2), Anthony Colaprete (1), Mihaly Horanyi (3), Paul Mahaffy (4), Butler Hine (1), Steven McClard (5), Joan Salute (6), Edwin Grayzeck (6), and Don Boroson (7) (1) NASA Ames Research Center, Moffett Field, CA USA ([email protected]), (2) Space Sciences Laboratory, University of California, Berkeley, CA USA, (3) Laboratory for Atmospheric and Space Physics, University of Colorado, Boulder, CO USA, (4) NASA Goddard Space Flight Center, Greenbelt, MD USA, (5) LunarQuest Program Office, NASA Marshall Space Flight Center, Huntsville, AL USA, (6) Planetary Science Division, Science Mission Directorate, NASA, Washington, DC USA, (7) Lincoln Laboratory, Massachusetts Institute of Technology, Lexington MA USA Nearly 40 years have passed since the last Apollo missions investigated the mysteries of the lunar atmosphere and the question of levitated lunar dust. The most important questions remain: what is the composition, structure and variability of the tenuous lunar exosphere? What are its origins, transport mechanisms, and loss processes? Is lofted lunar dust the cause of the horizon glow observed by the Surveyor missions and Apollo astronauts? How does such levitated dust arise and move, what is its density, and what is its ultimate fate? The US National Academy of Sciences/National Research Council decadal surveys and the recent “Scientific Context for Exploration of the Moon” (SCEM) reports have identified studies of the pristine state of the lunar atmosphere and dust environment as among the leading priorities for future lunar science missions.
    [Show full text]
  • USGS Open-File Report 2005-1190, Table 1
    TABLE 1 GEOLOGIC FIELD-TRAINING OF NASA ASTRONAUTS BETWEEN JANUARY 1963 AND NOVEMBER 1972 The following is a year-by-year listing of the astronaut geologic field training trips planned and led by personnel from the U.S. Geological Survey’s Branches of Astrogeology and Surface Planetary Exploration, in collaboration with the Geology Group at the Manned Spacecraft Center, Houston, Texas at the request of NASA between January 1963 and November 1972. Regional geologic experts from the U.S. Geological Survey and other governmental organizations and universities s also played vital roles in these exercises. [The early training (between 1963 and 1967) involved a rather large contingent of astronauts from NASA groups 1, 2, and 3. For another listing of the astronaut geologic training trips and exercises, including all attending and the general purposed of the exercise, the reader is referred to the following website containing a contribution by William Phinney (Phinney, book submitted to NASA/JSC; also http://www.hq.nasa.gov/office/pao/History/alsj/ap-geotrips.pdf).] 1963 16-18 January 1963: Meteor Crater and San Francisco Volcanic Field near Flagstaff, Arizona (9 astronauts). Among the nine astronaut trainees in Flagstaff for that initial astronaut geologic training exercise was Neil Armstrong--who would become the first man to step foot on the Moon during the historic Apollo 11 mission in July 1969! The other astronauts present included Frank Borman (Apollo 8), Charles "Pete" Conrad (Apollo 12), James Lovell (Apollo 8 and the near-tragic Apollo 13), James McDivitt, Elliot See (killed later in a plane crash), Thomas Stafford (Apollo 10), Edward White (later killed in the tragic Apollo 1 fire at Cape Canaveral), and John Young (Apollo 16).
    [Show full text]
  • No. 40. the System of Lunar Craters, Quadrant Ii Alice P
    NO. 40. THE SYSTEM OF LUNAR CRATERS, QUADRANT II by D. W. G. ARTHUR, ALICE P. AGNIERAY, RUTH A. HORVATH ,tl l C.A. WOOD AND C. R. CHAPMAN \_9 (_ /_) March 14, 1964 ABSTRACT The designation, diameter, position, central-peak information, and state of completeness arc listed for each discernible crater in the second lunar quadrant with a diameter exceeding 3.5 km. The catalog contains more than 2,000 items and is illustrated by a map in 11 sections. his Communication is the second part of The However, since we also have suppressed many Greek System of Lunar Craters, which is a catalog in letters used by these authorities, there was need for four parts of all craters recognizable with reasonable some care in the incorporation of new letters to certainty on photographs and having diameters avoid confusion. Accordingly, the Greek letters greater than 3.5 kilometers. Thus it is a continua- added by us are always different from those that tion of Comm. LPL No. 30 of September 1963. The have been suppressed. Observers who wish may use format is the same except for some minor changes the omitted symbols of Blagg and Miiller without to improve clarity and legibility. The information in fear of ambiguity. the text of Comm. LPL No. 30 therefore applies to The photographic coverage of the second quad- this Communication also. rant is by no means uniform in quality, and certain Some of the minor changes mentioned above phases are not well represented. Thus for small cra- have been introduced because of the particular ters in certain longitudes there are no good determi- nature of the second lunar quadrant, most of which nations of the diameters, and our values are little is covered by the dark areas Mare Imbrium and better than rough estimates.
    [Show full text]
  • General Index
    General Index Italicized page numbers indicate figures and tables. Color plates are in- cussed; full listings of authors’ works as cited in this volume may be dicated as “pl.” Color plates 1– 40 are in part 1 and plates 41–80 are found in the bibliographical index. in part 2. Authors are listed only when their ideas or works are dis- Aa, Pieter van der (1659–1733), 1338 of military cartography, 971 934 –39; Genoa, 864 –65; Low Coun- Aa River, pl.61, 1523 of nautical charts, 1069, 1424 tries, 1257 Aachen, 1241 printing’s impact on, 607–8 of Dutch hamlets, 1264 Abate, Agostino, 857–58, 864 –65 role of sources in, 66 –67 ecclesiastical subdivisions in, 1090, 1091 Abbeys. See also Cartularies; Monasteries of Russian maps, 1873 of forests, 50 maps: property, 50–51; water system, 43 standards of, 7 German maps in context of, 1224, 1225 plans: juridical uses of, pl.61, 1523–24, studies of, 505–8, 1258 n.53 map consciousness in, 636, 661–62 1525; Wildmore Fen (in psalter), 43– 44 of surveys, 505–8, 708, 1435–36 maps in: cadastral (See Cadastral maps); Abbreviations, 1897, 1899 of town models, 489 central Italy, 909–15; characteristics of, Abreu, Lisuarte de, 1019 Acequia Imperial de Aragón, 507 874 –75, 880 –82; coloring of, 1499, Abruzzi River, 547, 570 Acerra, 951 1588; East-Central Europe, 1806, 1808; Absolutism, 831, 833, 835–36 Ackerman, James S., 427 n.2 England, 50 –51, 1595, 1599, 1603, See also Sovereigns and monarchs Aconcio, Jacopo (d. 1566), 1611 1615, 1629, 1720; France, 1497–1500, Abstraction Acosta, José de (1539–1600), 1235 1501; humanism linked to, 909–10; in- in bird’s-eye views, 688 Acquaviva, Andrea Matteo (d.
    [Show full text]
  • Martian Crater Morphology
    ANALYSIS OF THE DEPTH-DIAMETER RELATIONSHIP OF MARTIAN CRATERS A Capstone Experience Thesis Presented by Jared Howenstine Completion Date: May 2006 Approved By: Professor M. Darby Dyar, Astronomy Professor Christopher Condit, Geology Professor Judith Young, Astronomy Abstract Title: Analysis of the Depth-Diameter Relationship of Martian Craters Author: Jared Howenstine, Astronomy Approved By: Judith Young, Astronomy Approved By: M. Darby Dyar, Astronomy Approved By: Christopher Condit, Geology CE Type: Departmental Honors Project Using a gridded version of maritan topography with the computer program Gridview, this project studied the depth-diameter relationship of martian impact craters. The work encompasses 361 profiles of impacts with diameters larger than 15 kilometers and is a continuation of work that was started at the Lunar and Planetary Institute in Houston, Texas under the guidance of Dr. Walter S. Keifer. Using the most ‘pristine,’ or deepest craters in the data a depth-diameter relationship was determined: d = 0.610D 0.327 , where d is the depth of the crater and D is the diameter of the crater, both in kilometers. This relationship can then be used to estimate the theoretical depth of any impact radius, and therefore can be used to estimate the pristine shape of the crater. With a depth-diameter ratio for a particular crater, the measured depth can then be compared to this theoretical value and an estimate of the amount of material within the crater, or fill, can then be calculated. The data includes 140 named impact craters, 3 basins, and 218 other impacts. The named data encompasses all named impact structures of greater than 100 kilometers in diameter.
    [Show full text]
  • PEANUTS and SPACE FOUNDATION Apollo and Beyond
    Reproducible Master PEANUTS and SPACE FOUNDATION Apollo and Beyond GRADE 4 – 5 OBJECTIVES PAGE 1 Students will: ö Read Snoopy, First Beagle on the Moon! and Shoot for the Moon, Snoopy! ö Learn facts about the Apollo Moon missions. ö Use this information to complete a fill-in-the-blank fact worksheet. ö Create mission objectives for a brand new mission to the moon. SUGGESTED GRADE LEVELS 4 – 5 SUBJECT AREAS Space Science, History TIMELINE 30 – 45 minutes NEXT GENERATION SCIENCE STANDARDS ö 5-ESS1 ESS1.B Earth and the Solar System ö 3-5-ETS1 ETS1.B Developing Possible Solutions 21st CENTURY ESSENTIAL SKILLS Collaboration and Teamwork, Communication, Information Literacy, Flexibility, Leadership, Initiative, Organizing Concepts, Obtaining/Evaluating/Communicating Ideas BACKGROUND ö According to NASA.gov, NASA has proudly shared an association with Charles M. Schulz and his American icon Snoopy since Apollo missions began in the 1960s. Schulz created comic strips depicting Snoopy on the Moon, capturing public excitement about America’s achievements in space. In May 1969, Apollo 10 astronauts traveled to the Moon for a final trial run before the lunar landings took place on later missions. Because that mission required the lunar module to skim within 50,000 feet of the Moon’s surface and “snoop around” to determine the landing site for Apollo 11, the crew named the lunar module Snoopy. The command module was named Charlie Brown, after Snoopy’s loyal owner. These books are a united effort between Peanuts Worldwide, NASA and Simon & Schuster to generate interest in space among today’s younger children.
    [Show full text]
  • Exploration of the Moon
    Exploration of the Moon The physical exploration of the Moon began when Luna 2, a space probe launched by the Soviet Union, made an impact on the surface of the Moon on September 14, 1959. Prior to that the only available means of exploration had been observation from Earth. The invention of the optical telescope brought about the first leap in the quality of lunar observations. Galileo Galilei is generally credited as the first person to use a telescope for astronomical purposes; having made his own telescope in 1609, the mountains and craters on the lunar surface were among his first observations using it. NASA's Apollo program was the first, and to date only, mission to successfully land humans on the Moon, which it did six times. The first landing took place in 1969, when astronauts placed scientific instruments and returnedlunar samples to Earth. Apollo 12 Lunar Module Intrepid prepares to descend towards the surface of the Moon. NASA photo. Contents Early history Space race Recent exploration Plans Past and future lunar missions See also References External links Early history The ancient Greek philosopher Anaxagoras (d. 428 BC) reasoned that the Sun and Moon were both giant spherical rocks, and that the latter reflected the light of the former. His non-religious view of the heavens was one cause for his imprisonment and eventual exile.[1] In his little book On the Face in the Moon's Orb, Plutarch suggested that the Moon had deep recesses in which the light of the Sun did not reach and that the spots are nothing but the shadows of rivers or deep chasms.
    [Show full text]
  • 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.
    [Show full text]
  • 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.
    [Show full text]
  • École De Paris Tableaux Modernes Photographies Aviation Conquête Spatiale
    EXPERTISES – VENTES AUX ENCHÈRES École de Paris Tableaux modernes Photographies Aviation Conquête spatiale Paris - Hôtel Drouot - 8 et 9 octobre 2019 EXPERTISES – VENTES AUX ENCHÈRES VENTE AUX ENCHÈRES PUBLIQUES Hôtel Drouot Richelieu salle 6 9, rue Drouot à Paris IXe Mardi 8 octobre 2019 à 14 h École de Paris Tableaux Modernes Mercredi 9 octobre 2019 à 14 h Photographies Aviation Conquête spatiale Reproduction des œuvres sur : www.ogerblanchet.fr - www.jj-mathias.fr Expositions publiques : Le lundi 7 octobre de 11 h à 18 heures Le mardi 8 octobre de 11 h à 12 heures Le mercredi 9 octobre de 11 h à 12 heures EXPERTISES – VENTES AUX ENCHÈRES 22 rue Drouot - 75009 Paris 01 42 46 96 95 - [email protected] ASSISTÉS DES EXPERTS Pour les lots 5 à 10 Pour l’École de Paris Éric SCHOELLER Christophe ZAGRODKI Tél. +33 (0)6 11 86 39 64 Tél. +33 (0)1 43 21 44 52 [email protected] [email protected] Pour les lots 38, 82 à 136, 252, 253, 281 à 287, Pour les autographes et manuscrits 289 à 314 M. Jean-Emmanuel RAUX Cabinet PERAZZONE-BRUN Arts et Autographes 4, rue Favart - 75002 9 rue de l’Odéon - 75006 Paris Tél. +33 (0)1 42 60 45 45 01 43 25 60 48 - [email protected] Pour les photographies M. Serge PLANTUREUX 80 Rue Taitbout - 75009 Paris Tél. +33 (0)6 50 85 60 74 - [email protected] AVERTISSEMENT Concernant l’état des œuvres décrites dans le présent catalogue, des rapports d’état sont disponibles sur simple demande Pour les estampes, sauf mention contraire, les dimensions sont celles de la cuvette pour les gravures et du sujet pour les lithographies J.J.
    [Show full text]
  • 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.
    [Show full text]