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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. -
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. -
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. -
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. -
Impact Cratering
6 Impact cratering The dominant surface features of the Moon are approximately circular depressions, which may be designated by the general term craters … Solution of the origin of the lunar craters is fundamental to the unravel- ing of the history of the Moon and may shed much light on the history of the terrestrial planets as well. E. M. Shoemaker (1962) Impact craters are the dominant landform on the surface of the Moon, Mercury, and many satellites of the giant planets in the outer Solar System. The southern hemisphere of Mars is heavily affected by impact cratering. From a planetary perspective, the rarity or absence of impact craters on a planet’s surface is the exceptional state, one that needs further explanation, such as on the Earth, Io, or Europa. The process of impact cratering has touched every aspect of planetary evolution, from planetary accretion out of dust or planetesimals, to the course of biological evolution. The importance of impact cratering has been recognized only recently. E. M. Shoemaker (1928–1997), a geologist, was one of the irst to recognize the importance of this process and a major contributor to its elucidation. A few older geologists still resist the notion that important changes in the Earth’s structure and history are the consequences of extraterres- trial impact events. The decades of lunar and planetary exploration since 1970 have, how- ever, brought a new perspective into view, one in which it is clear that high-velocity impacts have, at one time or another, affected nearly every atom that is part of our planetary system. -
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. -
A Study About the Temporal Constraints on the Martian Yardangs’ Development in Medusae Fossae Formation
remote sensing Article A Study about the Temporal Constraints on the Martian Yardangs’ Development in Medusae Fossae Formation Jia Liu 1,2 , Zongyu Yue 1,3,*, Kaichang Di 1,3 , Sheng Gou 1,4 and Shengli Niu 4 1 State Key Laboratory of Remote Sensing Science, Aerospace Information Research Institute, Chinese Academy of Sciences, Beijing 100101, China; [email protected] (J.L.); [email protected] (K.D.); [email protected] (S.G.) 2 University of Chinese Academy of Sciences, Beijing 100049, China 3 CAS Center for Excellence in Comparative Planetology, Hefei 230026, China 4 State Key Laboratory of Lunar and Planetary Sciences, Macau University of Science and Technology, Macau 999078, China; [email protected] * Correspondence: [email protected]; Tel.: +86-10-64889553 Abstract: The age of Mars yardangs is significant in studying their development and the evolution of paleoclimate conditions. For planetary surface or landforms, a common method for dating is based on the frequency and size distribution of all the superposed craters after they are formed. However, there is usually a long duration for the yardangs’ formation, and they will alter the superposed craters, making it impossible to give a reliable dating result with the method. An indirect method by analyzing the ages of the superposed layered ejecta was devised in the research. First, the layered ejecta that are superposed on and not altered by the yardangs are identified and mapped. Then, the ages of the layered ejecta are derived according to the crater frequency and size distribution on them. These ages indicate that the yardangs ceased development by these times, and the ages are valuable for studying the evolution of the yardangs. -
Apollo 13--200,000Miles from Earth
Apollo13"Houston,we'vegota problem." EP-76,ProducedbytheO fficeofPublicA ffairs NationalAeronauticsandSpaceAdministration W ashington,D.C.20546 U.S.GOVERNM ENT PRINTING OFFICE,1970384-459 NOTE:Nolongerinprint. .pdf version by Jerry Woodfill of the Automation, Robotics, and Simulation Division, Johnson Space Center, Houston, Texas 77058 . James A. Lovell, Jr., Commander... Fred W. Haise, Jr., Lunar Module Pilot... John L. Swigeft, Jr., Command Module Pilot. SPACECRAFT--Hey, we've got a problem here. Thus, calmly, Command Module Pilot JackSwigert gave the first intimation of serious trouble for Apollo 13--200,000miles from Earth. CAPSULECOMMUNICATOR--ThisisHouston;say again, please. SC--Houston, we've hada problem. We've hada MainBbusundervolt. By "undervolt"Swigert meant a drop in power in one of the Command/Service Module's two main electrical circuits. His report to the ground began the most grippingepisode in man's venture into space. One newspaper reporter called it the most public emergency and the most dramatic rescue in the history of exploration. SC--Andwe hada pretty large bang associatedwith the cautionandwarning here. Lunar Module Pilot Fred Haise was now on the voice channel from the spacecraft to the Mission Control Center at the National Aeronautics and Space Administration's Manned Spacecraft Center in Texas. Commander Jim Lovell would shortly be heard, then again Swigert--the backup crewman who had been thrust onto the first team only two days before launch when doctors feared that Tom Mattingly of the primary crew might come down with German measles. Equally cool, the men in Mission Control acknowledged the report and began the emergency procedures that grew into an effort by hundreds of ground controllers and thousands of technicians and scientists in NaSA contractor plants and On university campuses to solve the most complexand urgent problem yet encountered in space flight. -
Apollo Over the Moon: a View from Orbit (Nasa Sp-362)
chl APOLLO OVER THE MOON: A VIEW FROM ORBIT (NASA SP-362) Chapter 1 - Introduction Harold Masursky, Farouk El-Baz, Frederick J. Doyle, and Leon J. Kosofsky [For a high resolution picture- click here] Objectives [1] Photography of the lunar surface was considered an important goal of the Apollo program by the National Aeronautics and Space Administration. The important objectives of Apollo photography were (1) to gather data pertaining to the topography and specific landmarks along the approach paths to the early Apollo landing sites; (2) to obtain high-resolution photographs of the landing sites and surrounding areas to plan lunar surface exploration, and to provide a basis for extrapolating the concentrated observations at the landing sites to nearby areas; and (3) to obtain photographs suitable for regional studies of the lunar geologic environment and the processes that act upon it. Through study of the photographs and all other arrays of information gathered by the Apollo and earlier lunar programs, we may develop an understanding of the evolution of the lunar crust. In this introductory chapter we describe how the Apollo photographic systems were selected and used; how the photographic mission plans were formulated and conducted; how part of the great mass of data is being analyzed and published; and, finally, we describe some of the scientific results. Historically most lunar atlases have used photointerpretive techniques to discuss the possible origins of the Moon's crust and its surface features. The ideas presented in this volume also rely on photointerpretation. However, many ideas are substantiated or expanded by information obtained from the huge arrays of supporting data gathered by Earth-based and orbital sensors, from experiments deployed on the lunar surface, and from studies made of the returned samples. -
Glossary of Lunar Terminology
Glossary of Lunar Terminology albedo A measure of the reflectivity of the Moon's gabbro A coarse crystalline rock, often found in the visible surface. The Moon's albedo averages 0.07, which lunar highlands, containing plagioclase and pyroxene. means that its surface reflects, on average, 7% of the Anorthositic gabbros contain 65-78% calcium feldspar. light falling on it. gardening The process by which the Moon's surface is anorthosite A coarse-grained rock, largely composed of mixed with deeper layers, mainly as a result of meteor calcium feldspar, common on the Moon. itic bombardment. basalt A type of fine-grained volcanic rock containing ghost crater (ruined crater) The faint outline that remains the minerals pyroxene and plagioclase (calcium of a lunar crater that has been largely erased by some feldspar). Mare basalts are rich in iron and titanium, later action, usually lava flooding. while highland basalts are high in aluminum. glacis A gently sloping bank; an old term for the outer breccia A rock composed of a matrix oflarger, angular slope of a crater's walls. stony fragments and a finer, binding component. graben A sunken area between faults. caldera A type of volcanic crater formed primarily by a highlands The Moon's lighter-colored regions, which sinking of its floor rather than by the ejection of lava. are higher than their surroundings and thus not central peak A mountainous landform at or near the covered by dark lavas. Most highland features are the center of certain lunar craters, possibly formed by an rims or central peaks of impact sites. -
Appendix I Lunar and Martian Nomenclature
APPENDIX I LUNAR AND MARTIAN NOMENCLATURE LUNAR AND MARTIAN NOMENCLATURE A large number of names of craters and other features on the Moon and Mars, were accepted by the IAU General Assemblies X (Moscow, 1958), XI (Berkeley, 1961), XII (Hamburg, 1964), XIV (Brighton, 1970), and XV (Sydney, 1973). The names were suggested by the appropriate IAU Commissions (16 and 17). In particular the Lunar names accepted at the XIVth and XVth General Assemblies were recommended by the 'Working Group on Lunar Nomenclature' under the Chairmanship of Dr D. H. Menzel. The Martian names were suggested by the 'Working Group on Martian Nomenclature' under the Chairmanship of Dr G. de Vaucouleurs. At the XVth General Assembly a new 'Working Group on Planetary System Nomenclature' was formed (Chairman: Dr P. M. Millman) comprising various Task Groups, one for each particular subject. For further references see: [AU Trans. X, 259-263, 1960; XIB, 236-238, 1962; Xlffi, 203-204, 1966; xnffi, 99-105, 1968; XIVB, 63, 129, 139, 1971; Space Sci. Rev. 12, 136-186, 1971. Because at the recent General Assemblies some small changes, or corrections, were made, the complete list of Lunar and Martian Topographic Features is published here. Table 1 Lunar Craters Abbe 58S,174E Balboa 19N,83W Abbot 6N,55E Baldet 54S, 151W Abel 34S,85E Balmer 20S,70E Abul Wafa 2N,ll7E Banachiewicz 5N,80E Adams 32S,69E Banting 26N,16E Aitken 17S,173E Barbier 248, 158E AI-Biruni 18N,93E Barnard 30S,86E Alden 24S, lllE Barringer 29S,151W Aldrin I.4N,22.1E Bartels 24N,90W Alekhin 68S,131W Becquerei