Rex D. Hall and David J. Shayler
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2019 TS Q Intermediate
INTERMEDIATE Grades 8 and 9 NOT TO BE USED BEFORE 4 MARCH 2019 If you are NOT in grades 8 or 9, please report that you have the wrong paper. Only when the teacher says “START”, may you begin. 1. Write your personal details and your answers on the answer sheet provided. 2. You will have 45 minutes to complete the 15 tasks. 3. You may answer the questions in any order, but it is important to place the answer in the correct line on the answer sheet. 4. Leave the tasks you find difficult for later. The mark allocation is as follows: A section: +6 marks for every correct answer B section: +7 marks for every correct answer C section: +7 marks for every correct answer The maximum mark is 100. Wait for the teacher to say “START”. A1 Help Smiley Home A2 Lemonade Party Janet made 37 liters of lemonade at home and now she needs to put it in bottles to take it to school for a party. She has several empty bottles of various sizes, but she wants to use the smallest number of bottles AND all of the bottles have to be full. Task: Which bottles does she have to use? Write the answer in the correct block on your answer sheet as per example: 16+8+8+1= 33 A3 Mutation of an Alien An alien has a head, a body, two arms, and two legs. The alien can be mutated by using the following commands: (It is possible that the shape of a part is mutated more than once.) Mutasie Bevele H(C): change the head to , H(S): change the head to , H(T): change the head to B(C): change the body to , B(S): change the body to , B(T): change the body to A(+): make the arms long , A(-):make the arms short L(+): make the legs long , L(-):make the legs short Transformation example for H(S), B(S), A(-), L(-): Question: What will the alien look like after receiving the following commands? H(T), L(+), B(T), A(+), H(C), A(-), B(C) A B C D A4 Switch On Below you see a network of 7 light bulbs and 7 light switches. -
Raumstationen.Pdf
LARS WEILER ‹[email protected]› GPN14 – 19. JUNI 2014 RAUMSTATIONEN Bilder: NASA, ESA ÜBERSICHT • Motivation • Vorraussetzungen • Raumstationen • Zukunft MOTIVATION LEBEN IM WELTRAUM MOTIVATION FORSCHUNG ANFORDERUNGEN AN RAUMFAHRER VORRAUSSETZUNGEN ORBITING VORRAUSSETZUNGEN DOCKING VORRAUSSETZUNGEN DOCKING VORRAUSSETZUNGEN DOCKING VORRAUSSETZUNGEN DOCKING VORRAUSSETZUNGEN DOCKING RAUMSTATIONEN • Салют – Salyut • Skylab • Мир – Mir • Raumlabor • ISS/МКС • 天宫 一号 – Tiangong СССР – UDSSR САЛЮТ – SALYUT ДОС – Долговременная орбитальная станция (Langzeit-Orbital-Station) Алмаз – Almaz (Diamant) СССР – UDSSR САЛЮТ 1 – SALYUT 1 СССР – UDSSR АЛМАЗ – ALMAZ СССР – UDSSR САЛЮТ 4 – SALYUT 4 СССР – UDSSR САЛЮТ 6 – SALYUT 6 ТРАНСПОРТНЫЙ КОРАБЛЬ СНАБЖЕНИЯ ТКС – TKS СССР – UDSSR САЛЮТ 7 – SALYUT 7 СССР – UDSSR САЛЮТ 7 – SALYUT 7 USA – NASA SKYLAB USA – NASA SKYLAB USA – NASA SKYLAB СССР/РУССИЯ – UDSSR/RUSSLAND МИР – MIR DAS BAIKONUR-MYSTERIUM INKLINATION DAS BAIKONUR-MYSTERIUM INKLINATION МИР – MIR BESATZUNG MIRCORP ZEITGLEICH ZUR ISS МИР – MIR FEUER МИР – MIR KOLLISION МИР – MIR KOLLISION МИР – MIR VERSCHROTTUNG EUROPA – ESA / USA – NASA SPACELAB USA – NASA SPACEHAB РОСКОСМОС / NASA / ESA / JAXA / CSA ASC ISS / МКС ! INTERNATIONAL SPACE STATION ! МЕЖДУНАРОДНАЯ КОСМИЧЕСКАЯ СТАНЦИЯ ISS AUFBAU ISS ORBIT RAUMSCHIFFE СОЮЗ – SOYUZ RAUMSCHIFFE HERMES ISS TRASPORTFRACHTER DRAGON CARGO ISS TRASPORTFRACHTER DRAGON RETURN ISS TRASPORTFRACHTER ПРОГРЕСС – PROGRESS ISS TRASPORTFRACHTER ПРОГРЕСС – PROGRESS ISS TRANSPORTFRACHTER MPLM ISS TRANSPORTFRACHTER ATV ISS -
ORION ORION a to Z APOGEE to Break the Frangible Joints and Separate the Fairings, Three Parachutes
National Aeronautics and Space Administration ORION www.nasa.gov ORION A to Z APOGEE to break the frangible joints and separate the fairings, three parachutes. The next two parachutes will then VAN ALLEN RADIATION BELTS The term apogee refers to the point in an elliptical exposing the spacecraft to space. LAS - LAUNCH ABORT SYSTEM deploy and open. Once the spacecraft slows to around The Van Allen Belts are belts of plasma trapped by orbit when a spacecraft is farthest from the Earth. Orion’s Launch Abort System (LAS) is designed to 100 mph, the three main parachutes will then deploy the Earth’s magnetic field that shield the surface of During Exploration Flight Test-1, Orion’s flight path will GUPPY propel the crew module away from an emergency on using three pilot parachutes and slow the spacecraft the Earth from much of the radiation in space. During take it to an apogee of 3,600 miles. Just how high is The Super Guppy is a special airplane capable of the launch pad or during initial takeoff, moving the to around 20 mph for splashdown in the Pacific Ocean. Exploration Flight Test-1, Orion will pass within the Van that? A commercial airliner flies about 8 miles above transporting up to 26 tons in its cargo compartment crew away from danger. Orion’s LAS has three new When fully deployed, the canopies of three main Allen Radiation Belts and will spend more time in the the Earth’s surface, so Orion’s flight is 450 times farther measuring 25 feet tall, 25 feet wide, and 111 feet long. -
The Orbital-Hub: Low Cost Platform for Human Spaceflight After ISS
67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30 September 2016. Copyright ©2016 by the International Astronautical Federation (IAF). All rights reserved. IAC-16, B3,1,9,x32622 The Orbital-Hub: Low Cost Platform for Human Spaceflight after ISS O. Romberga, D. Quantiusa, C. Philpota, S. Jahnkea, W. Seboldta, H. Dittusb, S. Baerwaldeb, H. Schlegelc, M. Goldd, G. Zamkad, R. da Costae, I. Retate, R. Wohlgemuthe, M. Langee a German Aerospace Center (DLR), Institute of Space Systems, Bremen, Germany, [email protected] b German Aerospace Center (DLR), Executive Board, Space Research and Technology, Cologne, Germany, c European Space Agency (ESA) Contractor, Johnson Space Center, Houston, USA, d Bigelow Aerospace, Las Vegas / Washington, USA, e Airbus DS, Bremen, Germany Abstract The International Space Station ISS demonstrates long-term international cooperation between many partner governments as well as significant engineering and programmatic achievement mostly as a compromise of budget, politics, administration and technological feasibility. A paradigm shift to use the ISS more as an Earth observation platform and to more innovation and risk acceptance can be observed in the development of new markets by shifting responsibilities to private entities and broadening research disciplines, demanding faster access by users and including new launcher and experiment facilitator companies. A review of worldwide activities shows that all spacefaring nations are developing their individual programmes for the time after ISS. All partners are basically still interested in LEO and human spaceflight as discussed by the ISECG. ISS follow-on activities should comprise clear scientific and technological objectives combined with the long term view on space exploration. -
Installation, Care, and Maintenance of Wood Shake and Shingle Siding
United States Department of Agriculture Installation, Care, and Forest Service Maintenance of Wood Forest Products Laboratory Shake and Shingle Siding General Jack Dwyer Technical Report Tony Bonura FPL–GTR–202 Arnie Nebelsick Sam Williams Christopher G. Hunt Abstract Contents This article gives general guidelines for selection, instal- Introduction ......................................................................... 1 lation, finishing, and maintenance of wood shakes and Selection .............................................................................. 1 shingles. The authors gathered information from a variety of Shakes ............................................................................. 1 sources: research publications on wood finishing, technical data sheets from paint manufacturers, installation instruc- Shingles ........................................................................... 2 tions for shake and shingle siding, and interviews with Specialty Sidewall Products ............................................ 3 experts having experience constructing and inspecting shake Installation ........................................................................... 5 and shingle siding. If research reports could not be found, the recommendations are based on opinions of experts and Rain-Screen Method ....................................................... 5 practices that have been shown to give good service life for Direct Application ........................................................... 6 shakes and shingles. -
The First In-Flight Space Fatality
Quiz #001 Difficulty: Medium The First In-Flight Space Fatality 1. Which mission had the first in-flight 8. Which pilot was the mission backup? space fatality? A) Vladimir Titov S A) Soyuz-1 B) Yuri Gagarin B) Space Shuttle Challenger C) Sergei Gonchar C) Apollo13 P 9. Where was Col. Komarov buried? A 2. How old was Colonel Vladimir A) On a hill overlooking Moscow Komarov at the time of this mission? B) In a wall at the Kremlin C A) 30 C) At an undisclosed location B) 35 E C) 40 Answers: 3. Why did the mission fail? 1. (A) The mission took place April 23-24, A) The oxygen tank exploded 1967, and killed the pilot and only crew H B) The parachute did not open member, Colonel Vladimir Komarov. C) The heat shield was damaged 2. (C) I 3. (B) The main parachute did not release 4. What was the pilot doing minutes and the manually-deployed reserve chute S tangled with the main’s drogue. The before the crash? Soyuz-1 descent module hit the ground at T A) Screaming at mission control around 40 meters per second (89mph). B) Saying good-bye to his wife 4. (C) C) Preparing for landing 5. (A) It was the first crewed flight of the O Soyuz launch 7K-OK spacecraft and Soyuz 5. What was the purpose of the flight? rocket. The Soyuz-2 mission was aborted R before launch, after the 13th orbit of A) Dock with another vehicle and Soyuz-1. Y exchange crew in flight 6. -
View / Download
www.arianespace.com www.starsem.com www.avio Arianespace’s eighth launch of 2021 with the fifth Soyuz of the year will place its satellite passengers into low Earth orbit. The launcher will be carrying a total payload of approximately 5 518 kg. The launch will be performed from Baikonur, in Kazakhstan. MISSION DESCRIPTION 2 ONEWEB SATELLITES 3 Liftoff is planned on at exactly: SOYUZ LAUNCHER 4 06:23 p.m. Washington, D.C. time, 10:23 p.m. Universal time (UTC), LAUNCH CAMPAIGN 4 00:23 a.m. Paris time, FLIGHT SEQUENCES 5 01:23 a.m. Moscow time, 03:23 a.m. Baikonur Cosmodrome. STAKEHOLDERS OF A LAUNCH 6 The nominal duration of the mission (from liftoff to separation of the satellites) is: 3 hours and 45 minutes. Satellites: OneWeb satellite #255 to #288 Customer: OneWeb • Altitude at separation: 450 km Cyrielle BOUJU • Inclination: 84.7degrees [email protected] +33 (0)6 32 65 97 48 RUAG Space AB (Linköping, Sweden) is the prime contractor in charge of development and production of the dispenser system used on Flight ST34. It will carry the satellites during their flight to low Earth orbit and then release them into space. The dedicated dispenser is designed to Flight ST34, the 29th commercial mission from the Baikonur Cosmodrome in Kazakhstan performed by accommodate up to 36 spacecraft per launch, allowing Arianespace and its Starsem affiliate, will put 34 of OneWeb’s satellites bringing the total fleet to 288 satellites Arianespace to timely deliver the lion’s share of the initial into a near-polar orbit at an altitude of 450 kilometers. -
Soviet Steps Toward Permanent Human Presence in Space
SALYUT: Soviet Steps Toward Permanent Human Presence in Space December 1983 NTIS order #PB84-181437 Recommended Citation: SALYUT: Soviet Steps Toward Permanent Human Presence in Space–A Technical Mere- orandum (Washington, D. C.: U.S. Congress, Office of Technology Assessment, OTA- TM-STI-14, December 1983). Library of Congress Catalog Card Number 83-600624 For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402 Foreword As the other major spacefaring nation, the Soviet Union is a subject of interest to the American people and Congress in their deliberations concerning the future of U.S. space activities. In the course of an assessment of Civilian Space Stations, the Office of Technology Assessment (OTA) has undertaken a study of the presence of Soviets in space and their Salyut space stations, in order to provide Congress with an informed view of Soviet capabilities and intentions. The major element in this technical memorandum was a workshop held at OTA in December 1982: it was the first occasion when a significant number of experts in this area of Soviet space activities had met for extended unclassified discussion. As a result of the workshop, OTA prepared this technical memorandum, “Salyut: Soviet Steps Toward Permanent Human Presence in Space. ” It has been reviewed extensively by workshop participants and others familiar with Soviet space activities. Also in December 1982, OTA wrote to the U. S. S. R.’s Ambassador to the United States Anatoliy Dobrynin, requesting any information concerning present and future Soviet space activities that the Soviet Union judged could be of value to the OTA assess- ment of civilian space stations. -
North American Air Defense Command (NORAD), Weekly Intelligence Review (WIR), April 28, 1967
. ' DECLASSIFIED UNDER AUTHORITY OF THE INTERAGENCY SECURITY CLASSIFICATION APPEALS PANEL, E.O. l3526, SECTION 5.3(b)(3) ISCAP APPEAL NO. 2009-068, document no. 174 DECLASSIFICATION DATE: February 25,2015 ~ ,li, _ Ul (') • > ~ ~AND UBRARY · -- ~ ~ a. j ·_ REC'D. MAY 1 1561 fJd J I . ~ > n Q 3 4 '· . FOR OFFtCillt USE ONtV I · APR 2 9 \SG1 NOR AD a~· "-.} Issue No. 17/67, 28 April 1967 .I The WIR ·in Brigf ~----------------------~ r---~----~~L-----~------~---. f . !I + Portion identified as non ' 'I responsive to the appeal 5 Portion identified as non responsive to the appeal • 5 6 HECC£ C OSMOS l '>5 D E-OR LllTF.D J\lr.nost ~ . ncrly 8 <J\·qr~ a fte r launch. -D .Ff'lCULTlES WI TH SOY U7. 1 CAtS£ ABO RT OF S~HEDULEDSPECTAC~LAR M~irl Oll:iSloo prob;l.hly wa~ t{? tt·:t t~t~ f t::r COiirnonae.t. s . l.A1JJ'lCH WiNDOW F OC{ V ENUS OPENS IN MAY : So·.,.. let ru ,~ kct :. ( ~ u r breaking thl"'ough SOV l2T L:\IJ .'ICH( f~S i DE OJ\'I A B L ~; 3 <: lal,td cove:· (Sovit!t 1>r <t,.;r ) (OFFICJ.A L fv\ a.t ., Winci )•,y h i'l>;a.H.:J(l d ~a.rl!& r tb hi ye4r , for U'SF; ONfJY I (i r Ht time >in~.:~> !960, NOTE: P11g c!< l tl , 2'0 1 ZI , 2·• and Z5 9f rhio int~ u~ :1 :: c b,lAl'ik. _....... - - . - . - ... ~ ' .. ~ ' . ! •..,,'. ~ I .WIR to be Smaller Tempprarily -, ..... ~ _ "'J ~ Budgetary res\rictions on printing forces thew IR to pare doWh its size for the rest Qf the fiscal I year, which ends 3d June 1961. -
Trade Studies Towards an Australian Indigenous Space Launch System
TRADE STUDIES TOWARDS AN AUSTRALIAN INDIGENOUS SPACE LAUNCH SYSTEM A thesis submitted for the degree of Master of Engineering by Gordon P. Briggs B.Sc. (Hons), M.Sc. (Astron) School of Engineering and Information Technology, University College, University of New South Wales, Australian Defence Force Academy January 2010 Abstract During the project Apollo moon landings of the mid 1970s the United States of America was the pre-eminent space faring nation followed closely by only the USSR. Since that time many other nations have realised the potential of spaceflight not only for immediate financial gain in areas such as communications and earth observation but also in the strategic areas of scientific discovery, industrial development and national prestige. Australia on the other hand has resolutely refused to participate by instituting its own space program. Successive Australian governments have preferred to obtain any required space hardware or services by purchasing off-the-shelf from foreign suppliers. This policy or attitude is a matter of frustration to those sections of the Australian technical community who believe that the nation should be participating in space technology. In particular the provision of an indigenous launch vehicle that would guarantee the nation independent access to the space frontier. It would therefore appear that any launch vehicle development in Australia will be left to non- government organisations to at least define the requirements for such a vehicle and to initiate development of long-lead items for such a project. It is therefore the aim of this thesis to attempt to define some of the requirements for a nascent Australian indigenous launch vehicle system. -
Limitations of Spacecraft Redundancy: a Case Study Analysis
44th International Conference on Environmental Systems Paper Number 13-17 July 2014, Tucson, Arizona Limitations of Spacecraft Redundancy: A Case Study Analysis Robert P. Ocampo1 University of Colorado Boulder, Boulder, CO, 80309 Redundancy can increase spacecraft safety by providing the crew or ground with multiple means of achieving a given function. However, redundancy can also decrease spacecraft safety by 1) adding additional failure modes to the system, 2) increasing design “opaqueness”, 3) encouraging operational risk, and 4) masking or “normalizing” design flaws. Two Loss of Crew (LOC) events—Soyuz 11 and Challenger STS 51-L—are presented as examples of these limitations. Together, these case studies suggest that redundancy is not necessarily a fail-safe means of improving spacecraft safety. I. Introduction A redundant system is one that can achieve its intended function through multiple independent pathways or Aelements 1,2. In crewed spacecraft, redundancy is typically applied to systems that are critical for safety and/or mission success3,4. Since no piece of hardware can be made perfectly reliable, redundancy—in theory—allows for the benign (e.g. non-catastrophic) failure of critical elements. Redundant elements can be 1) similar or dissimilar to each other, 2) activated automatically (“hot spare”) or manually (“cold spare”), and 3) located together or separated geographically5-7. U.S. spacecraft have employed redundancy on virtually all levels of spacecraft design, from component to subsystem7,8. Redundancy has a successful history of precluding critical and catastrophic failures during human spaceflight. A review of NASA mission reports, from Mercury to Space Shuttle, indicates that redundancy has saved the crew or extended the mission over 160 times, or roughly once per flight9. -
The Soviet Space Program
C05500088 TOP eEGRET iuf 3EEA~ NIE 11-1-71 THE SOVIET SPACE PROGRAM Declassified Under Authority of the lnteragency Security Classification Appeals Panel, E.O. 13526, sec. 5.3(b)(3) ISCAP Appeal No. 2011 -003, document 2 Declassification date: November 23, 2020 ifOP GEEAE:r C05500088 1'9P SloGRET CONTENTS Page THE PROBLEM ... 1 SUMMARY OF KEY JUDGMENTS l DISCUSSION 5 I. SOV.IET SPACE ACTIVITY DURING TfIE PAST TWO YEARS . 5 II. POLITICAL AND ECONOMIC FACTORS AFFECTING FUTURE PROSPECTS . 6 A. General ............................................. 6 B. Organization and Management . ............... 6 C. Economics .. .. .. .. .. .. .. .. .. .. .. ...... .. 8 III. SCIENTIFIC AND TECHNICAL FACTORS ... 9 A. General .. .. .. .. .. 9 B. Launch Vehicles . 9 C. High-Energy Propellants .. .. .. .. .. .. .. .. .. 11 D. Manned Spacecraft . 12 E. Life Support Systems . .. .. .. .. .. .. .. .. 15 F. Non-Nuclear Power Sources for Spacecraft . 16 G. Nuclear Power and Propulsion ..... 16 Te>P M:EW TCS 2032-71 IOP SECl<ET" C05500088 TOP SECRGJ:. IOP SECREI Page H. Communications Systems for Space Operations . 16 I. Command and Control for Space Operations . 17 IV. FUTURE PROSPECTS ....................................... 18 A. General ............... ... ···•· ................. ····· ... 18 B. Manned Space Station . 19 C. Planetary Exploration . ........ 19 D. Unmanned Lunar Exploration ..... 21 E. Manned Lunar Landfog ... 21 F. Applied Satellites ......... 22 G. Scientific Satellites ........................................ 24 V. INTERNATIONAL SPACE COOPERATION ............. 24 A. USSR-European Nations .................................... 24 B. USSR-United States 25 ANNEX A. SOVIET SPACE ACTIVITY ANNEX B. SOVIET SPACE LAUNCH VEHICLES ANNEX C. SOVIET CHRONOLOGICAL SPACE LOG FOR THE PERIOD 24 June 1969 Through 27 June 1971 TCS 2032-71 IOP SLClt~ 70P SECRE1- C05500088 TOP SEGR:R THE SOVIET SPACE PROGRAM THE PROBLEM To estimate Soviet capabilities and probable accomplishments in space over the next 5 to 10 years.' SUMMARY OF KEY JUDGMENTS A.