Orders of Magnitude (Acceleration) - Wikipedia

Total Page:16

File Type:pdf, Size:1020Kb

Orders of Magnitude (Acceleration) - Wikipedia 10/08/2018 Orders of magnitude (acceleration) - Wikipedia Orders of magnitude (acceleration) This page lists examples of the acceleration occurring in various situations. They are grouped by orders of magnitude. https://en.wikipedia.org/wiki/Orders_of_magnitude_(acceleration) 1/6 10/08/2018 Orders of magnitude (acceleration) - Wikipedia Factor Reference Multiple Value [g] Item [m/s2] frame The gyro rotors in Gravity Probe B and the free-floating inertial 2 0 g 0 m/s proof masses in the TRIAD I navigation satellite[1] Weightless parabola in a inertial ≈ 0 m/s2 ≈ 0 g reduced-gravity aircraft Smallest acceleration in a lab 5 × 10−14 m/s2 5 × 10−15 g scientific experiment[2] 100 1 m/s2 lab 0.25 m/s2 0.026 g Train acceleration for SJ X2 Standing on the Moon at its inertial 1.62 m/s2 0.1652 g equator Car acceleration 0–100 km/h lab 4.3 m/s2 0.44 g in 6.4 s with a Saab 9-5 Hirsch Standard gravity, the gravity inertial 9.80665 m/s2 1 g acceleration on Earth at sea level standard[3] 1 2 Saturn V moon rocket just 10 1 dam/s inertial 11.2 m/s2 1.14 g after launch Bugatti Veyron from 0 to 100 km/h in 2.4 s (the net acceleration vector including inertial 15.2 m/s2 1.55 g gravitational acceleration is directed 40 degrees from horizontal) Space Shuttle, maximum inertial 29 m/s2 3 g during launch and reentry Sustainable for > 25 seconds, inertial 29 m/s2 3 g for a human[3] inertial 34 – 62 m/s2 3.5 – 6.3 g High-G roller coasters[4]:340 Top Fuel drag racing world lab? 41 m/s2 4.2 g record of 4.4 s over 1/4 mile Causes disorientation, inertial 49 m/s2 5 g dizziness and fainting in humans[3] Formula One car, maximum lab? 49+ m/s2 5+ g under heavy braking Luge, maximum expected at inertial? 51 m/s2 5.2 g the Whistler Sliding Centre Formula One car, peak lateral lab 49 – 59 m/s2 5 – 6 g in turns[5] Parachutist peak during inertial 59 m/s2 6 g normal opening of parachute[6] Standard, full aerobatics inertial +69 / -49 m/s2 +7 / -5 g certified glider inertial 70.6 m/s2 7.19 g Apollo 16 on reentry[7] inertial 79 m/s2 8 g F-16 aircraft pulling out of dive inertial 88 m/s2 9 g Maximum for a fit, trained person with G-suit to keep https://en.wikipedia.org/wiki/Orders_of_magnitude_(acceleration) 2/6 10/08/2018 Orders of magnitude (acceleration) - Wikipedia consciousness, avoiding G- LOC Typical maximum turn inertial 88 – 118 m/s2 9 – 12 g acceleration in an aerobatic plane or fighter jet[8] Explosive seat ejection from 147 m/s2 15 g aircraft Physical damage in humans 177 m/s2 18 g like broken capillaries[3] Peak acceleration 209 m/s2 21.3 g experienced by cosmonauts during the Soyuz 18a abort[9] Peak deceleration of the 333 m/s2 34 g Stardust Sample Return Capsule on reentry to Earth[10] 102 1 hm/s2 inertial Maximum acceleration a 454 m/s2 46.2 g human has survived on a rocket sled[3] > 491 m/s2 > 50 g Death or serious injury likely 982 m/s2 100 g Sprint missile[11] Automobile crash (100 km/h 982 m/s2 100 g into wall)[12] Brief human exposure > 982 m/s2 > 100 g survived in crash[13] 982 m/s2 100 g Deadly limit for most humans Peak acceleration of fastest 1540 m/s2 157 g rocket sled run[14] 3.5" hard disc non-operating 1964 m/s2 200 g shock tolerance for 2 ms, weight 0.6 kg[15] Peak deceleration inertial 103 1 km/s2 experienced by Jules Bianchi ≈ lab 2 254 g 2490 m/s in crash of Marussia MR03, 2014 Japanese Grand Prix[16] 2946 m/s2 300 g Soccer ball struck by foot 3200 m/s2 320 g A jumping human flea[17] 3800 m/s2 380 g A jumping click beetle[18] 104 10 km/s2 Deceleration of the head of a 11 768 m/s2 1200 g woodpecker[19] Space gun with a barrel length of 1 km and a muzzle velocity of 6 km/s, 17 680 m/s2 1800 g as proposed by Quicklaunch (assuming constant acceleration) 29460 m/s2 3000 g Baseball struck by bat[12] Shock capability of >49 100 m/s2 > 5000 g mechanical wrist watches[20] 84 450 m/s2 8600 g Current Formula One engines, maximum piston https://en.wikipedia.org/wiki/Orders_of_magnitude_(acceleration) 3/6 10/08/2018 Orders of magnitude (acceleration) - Wikipedia acceleration[21] 102 000 m/s2 10 400 g A mantis shrimp punch[22] Rating of electronics built into 152 210 m/s2 15 500 g military artillery shells[23] 100 105 Spore acceleration of the km/s2 196 400 m/s2 20 000 g Pilobolus fungi[24] 9×19mm Parabellum handgun 304 420 m/s2 31 000 g bullet (average along the length of the barrel)[25] Closing jaws of a trap-jaw 1 000 000 m/s2 100 000 g ant[26] 2 9×19mm Parabellum handgun 1 865 800 m/s 190 000 g [27] 106 1 Mm/s2 bullet, peak Surface gravity of white dwarf 3 800 000 m/s2 390 000 g Sirius B[28] 3 900 000 m/s2 slightly below 400 000 g Ultracentrifuge[29] 107 10 Mm/s2 53 000 000 m/s2 5 400 000 g Jellyfish stinger[30] Max surface gravity of a 7 × 1012 m/s2 7 × 1011 g neutron star 1012 1 Tm/s2 Protons in the Large Hadron 2.1 × 1013 m/s2 2.1 × 1012 g Collider[31] Classical (Bohr model) 9.149 × 1021 m/s2 9.33 × 1020 g acceleration of an electron around a H nucleus. 1021 1 Zm/s2 1 Electrons in a 1 TV/m 176 × 1021 m/s2 1.79 × 1022 g wakefield accelerator[32] 1051 1051 m/s2 5.561 × 1051 m/s2 5.67 × 1050 g Planck acceleration[33] See also G-force Gravitational acceleration Mechanical shock Standard gravity International System of Units (SI) SI prefix References 1. Stanford University: Gravity Probe B, Payload & Spacecraft (http://einstein.stanford.edu/TECH/technology2.html), and NASA: Investigation of Drag-Free Control Technology for Earth Science Constellation Missions (http://esto.na sa.gov/files/2002/Drag-Free%20Technology/DFC_ESTO_final_97.pdf). The TRIAD 1 satellite was a later, more advanced navigation satellite that was part of the U.S. Navy’s Transit, or NAVSAT system. 2. http://journals.aps.org/prl/abstract/10.1103/PhysRevLett.98.150801 3. csel.eng.ohio-state.edu - High Acceleration and the Human Body, Martin Voshell, November 28, 2004 (http://csel. eng.ohio-state.edu/voshell/gforce.pdf) Archived (https://web.archive.org/web/20140819225557/http://csel.eng.ohi o-state.edu/voshell/gforce.pdf) August 19, 2014, at the Wayback Machine. 4. George Bibel. Beyond the Black Box: the Forensics of Airplane Crashes. Johns Hopkins University Press, 2008. ISBN 0-8018-8631-7. https://en.wikipedia.org/wiki/Orders_of_magnitude_(acceleration) 4/6 10/08/2018 Orders of magnitude (acceleration) - Wikipedia 5. 6 g has been recorded in the 130R turn at Suzuka circuit, Japan. [1] (http://www.formula1.com/news/headlines/20 09/9/10005.html) Many turns have 5 g peak values, like turn 8 at Istanbul or Eau Rouge at Spa 6. http://www.pcprg.com/g-forces.htm 7. NASA: SP-368 Biomedical Results of Apollo, Chapter 5: Environmental Factors, Table 2: Apollo Manned Space Flight Reentry G Levels (https://history.nasa.gov/SP-368/s2ch5.htm) 8. "Maxed out: How many gs can you pull?" (https://www.newscientist.com/article/mg20627562-200-maxed-out-how -many-gs-can-you-pull/). New Scientist. Retrieved 2017-11-19. 9. Hall, Rex; David Shayler (2003). Soyuz, A Universal Spacecraft. Springer Praxis. p. 193. ISBN 1-85233-657-9. 10. ReVelle, D. O.; Edwards, W. N. (2007). "Stardust—An artificial, low-velocity "meteor" fall and recovery: 15 January 2006" (http://onlinelibrary.wiley.com/doi/10.1111/j.1945-5100.2007.tb00232.x/pdf) (PDF). The Meteoritical Society. 11. Sprint (http://www.nuclearabms.info/Sprint.html) 12. tomshardware.co.uk - Hard Drive Shock Tolerance - Hard-Disks - Storage (http://www.tomshardware.co.uk/forum/ 216253-14-hard-drive-shock-tolerance), Physics, by O'hanian, 1989, 2007-01-03 13. “Several Indy car drivers have withstood impacts in excess of 100 G without serious injuries.” Dennis F. Shanahan, M.D., M.P.H.: ”Human Tolerance and Crash Survivability (ftp://ftp.rta.nato.int/PubFullText/RTO/EN/RT O-EN-HFM-113/EN-HFM-113-06.pdf), citing Society of Automotive Engineers. Indy racecar crash analysis. Automotive Engineering International, June 1999, 87–90. And National Highway Traffic Safety Administration: Recording Automotive Crash Event Data (http://www.nhtsa.dot.gov/cars/problems/studies/record/chidester.htm) 14. http://www.holloman.af.mil/library/factsheets/factsheet_print.asp?fsID=6130&page=1 15. wdc.com - Legacy Product Specifications : WD600BB (http://www.wdc.com/en/products/legacy/Legacy.asp?Mode l=WD600BB), read 2012-01-11 16. "Formula 1 - Bianchi crash impact was 254g" (https://web.archive.org/web/20150723230530/https://uk.eurosport.y ahoo.com/news/formula-1-bianchi-crash-impact-254g-103939864--f1.html). uk.eurosport.yahoo.com. 23 July 2015. Archived from the original (https://uk.eurosport.yahoo.com/news/formula-1-bianchi-crash-impact-254g-1039 39864--f1.html) on 23 July 2015.
Recommended publications
  • Interstellar Travel Or Even 1.3 Mlbs at Launch
    Terraforming Mars: By Aliens? Astronomy 330 •! Sometime movies are full of errors. •! But what can you do? Music: Rocket Man– Elton John Online ICES Question •! ICES forms are available online, so far 39/100 Are you going to fill out an ICES form before the students have completed it. deadline? •! I appreciate you filling them out! •! Please make sure to leave written comments. I a)! Yes, I did it already. find these comments the most useful, and typically b)! Yes, sometime today that’s where I make the most changes to the c)! Yes, this weekend course. d)! Yes, I promise to do it before the deadline of May6th! e)! No, I am way too lazy to spend 5 mins to help you or future students out. Final Final •! In this classroom, Fri, May 7th, 0800-1100. •! A normal-sized sheet of paper with notes on both •! Will consist of sides is allowed. –! 15 question on Exam 1 material. •! Exam 1and 2 and last year’s final are posted on –! 15 question on Exam 2 material. class website (not Compass). –! 30 questions from new material (Lect 20+). –! +4 extra credit questions •! I will post a review sheet Friday. •! A total of 105 points, i.e. 5 points of extra credit. •! Final Exam grade is based on all three sections. •! If Section 1/2 grade is higher than Exam 1/2 grade, then it will replace your Exam 1/2 grade. Final Papers Outline •! Final papers due at BEGINNING of discussion •! Rockets: how to get the most bang for the buck.
    [Show full text]
  • Engineering 8 Launch Vehicles
    Papers on the Lunar Settlement Engineering 8 : Launch Vehicles mass of each stage is 10% the fuel mass, 0. Introduction This paper since the larger lower stages will be accompanies number 03-01 on the more structurally efficient but must bear logistics of space access. It is intended the load of the upper stages. to present technical analysis of relevant concepts, specifically the expendable If the required velocity increment for multistage rocket for direct ascent, the direct ascent, without an intermediate single-stage reusable terrestrial orbiter, orbit, is taken as the sum of the escape two-stage reusable and partially reusable velocities of Terra and Luna, 13.6 km/s, configurations, the lunar rocket, and the the necessary mass ratio with exhaust space gun. At this early date, however, velocity 4.0 km/s is 30. This sets the nothing more than approximations and maximum delivered mass at 33 t, and general considerations can be furnished. indicates that several steps are required. While specific numerical values are As a little calculation will show, the indicated in certain places, it must be overall efficiency of a step rocket is understood clearly that few of these have improved by using low mass-ratios in any validity ; they are presented in order the lower steps. We may select a to indicate trends of expected behaviour. tristage configuration, with step mass ratios of 2, 3, and 5. 1. Expendable Rocket For the expendable rocket to be useful, it must The mass of the first step, then, is 550 t, be very large. Two factors are at work of which 500 t is fuel ; the second, 330 t, here : first, ceteris paribus , the larger with 300 t fuel ; and the third is the the rocket, the larger the useful mass lunar-landing stage, 120 t with 96 t fuel.
    [Show full text]
  • This Third Edition Bibliography Lists Books and Teaching Aids Related To
    60:CUMENT RESUMB ED 027 215 SE 006 287 Aerospace Bibliography, Third Edition. National Aeronautics and Space Administration, Washingtan, D.C. Repor t No- EP -35 Pub Date (651 Note-68p. EDRS Price f1F-$0.50 HC-$3.50 Descriptors-*Aerospace Technok)gy, *Annotated Bibliographies, Astronomy, *Bibliographies, Physical Sciences, *Science Education, Technology Identifiers-National Aeronautics and Space Administration Thisthirdeditionbibliographylistsbooks and teaching aids related to aeronautics and space. Aeronautics titles are limited toaerospace-related research subjects, and books on astronomy to those direCtly related to space exploration. Also listed are pertinent references like pamphlets, films,film strips, booklets, charts, pictures, periodicals, and sources of in.formation on specific space subjects available from aerospace industry companies. Reading levels for each document are indicated according to primary, intermediate, upper elementary, secondary, and adult or college. (GR) 33' $ t 'k 4 ;(' " ; , othisit-erP-ie I l if= WIN IP , ., k a k ' II U.S. DEPARTMENT OF HEALTH, EDUCATION & WELFARE OFFICE OF EDUCATION THIS DOCUMENT HAS BEEN REPRODUCED EXACTLY AS RECEIVED FROM THE PERSON OR ORGANIZATION ORIGINATING IT.POINTS OF VIEW OR OPINIONS STATED DO NOT NECESSARILY REPRESENT OFF!CIAL OFFICE OF EDUCATION POSITION OR POLICY. 0 ,"'". Al 1011011104- 1,," 1. 1,=z;z0z2i Ent AEROSPACE BIBLIOGRAPHY THIRD EDITION Compiled for Educational Programs Division, Office of Public Affairs NATIONAL AERONAUTICS AND SPACE ADMINISTRATION by National Aerospace
    [Show full text]
  • Call for Papers Abstract Deadline 7 December 2015
    JANNAF INTERAGENCY PROPULSION COMMITTEE JOINT ARMY-NAVY-NASA-AIR FORCE 63rd JANNAF Propulsion Meeting Programmatic and Industrial Base Meeting 47th Combustion (CS) 35th Airbreathing Propulsion (APS) 35th Exhaust Plume and Signatures (EPSS) 29th Propulsion Systems Hazards (PSHS) JOINT SUBCOMMITTEE MEETING 16 - 20 May 2016 Announcement and Call For Papers Abstract Deadline 7 December 2015 Newport News, Virginia last updated 1/27/16 The May 2016 meeting of the Joint Army-Navy-NASA-Air SCOPE Force (JANNAF) will consist of the 63rd JANNAF Propulsion meeting; the Programmatic and Industrial Base (PIB) JANNAF Propulsion Meeting meeting; and the Joint Meeting of the 47th Combustion / The JANNAF Propulsion Meeting (JPM) encompasses research 35th Airbreathing Propulsion / 35th Exhaust Plume and and applications at the systems level. The JPM is held each Signatures / 29th Propulsion Systems Hazards Subcommittees. year in conjunction with standing JANNAF subcommittee Dr. Christine M. Michienzie with OSD (AT&L), MIBP, meetings on a rotating basis. The scope of the 63rd JPM in Alexandria, Virginia, is the meeting chair. This meeting will 2016 spans eight mission areas: Tactical Propulsion; Missile be held Monday through Friday, 16 - 20 May 2016, at the Defense/Strategic Propulsion; Propulsion Systems for Space Newport News Marriott at City Center in Newport News, Access; Gun and Gun-Launched Propulsion; Propulsion and Virginia. Please refer to page 4 for hotel and area information. Energetics Test Facilities; Sensors for Propulsion Measurement Applications;
    [Show full text]
  • To Orbit and Back Again: How the Space Shuttle Flew in Space Free Download
    TO ORBIT AND BACK AGAIN: HOW THE SPACE SHUTTLE FLEW IN SPACE FREE DOWNLOAD Davide Sivolella | 524 pages | 09 Sep 2013 | Springer-Verlag New York Inc. | 9781461409823 | English | New York, NY, United States To Orbit and Back Again: How the Space Shuttle Flew in Space (Springer… Details of how anomalous events were dealt with on individual missions are also provided, as are the recollections of those who built and flew the Shuttle. He involves here few in photographers on: electoral antitrust exceptionalism; teriparatide and significant experience; concept and matters; and s Futurism. Orbiting skyhooks Skyhook Momentum exchange tether. Soviet X-planes. This passion for astronautics led to bacheklor's and master's degrees in Aerospace Engineering from the Polytechnic of Turin Italy. Archived from the original on 26 June Technical material has been obtained from NASA as well as from other forums and specialists. The Rockwell X National Aero-Space Plane NASPbegun in the s, was an attempt to build a scramjet vehicle capable of operating like an aircraft and achieving orbit like the shuttle. InNASA originally planned to have the Gemini spacecraft land on a runway [18] with a Rogallo wing airfoilrather than an ocean landing under parachutes. Namespaces Article Talk. The spaceplane was also intended to carry cargo, with both upmass and downmass capacity. Search icon An illustration of a magnifying glass. Orbital spaceplanes are more like spacecraft, while sub-orbital spaceplanes are more like fixed-wing aircraft. Our configurations are tall Bodies and genotypes on which to See your new nationality. Space Policy. Details of how anomalous events were dealt with on individual missions are also provided, as are the recollections of those who built and flew the Shuttle.
    [Show full text]
  • Making-Space-For-Security-En-346.Pdf
    TABLE OF CONTENTS Editor's Note Kerstin VIGNARD ............................................................................................................. 1 Special Comment Colonel Chris A. HADFIELD .............................................................................................. 3 Making Space for Security? ‘Peaceful uses’ of outer space has permitted its militarization— does it also mean its weaponization? Johannes M. WOLFF......................................................................................................... 5 Monsters and shadows: left unchecked, American fears regarding threats to space assets will drive weaponization Theresa HITCHENS ........................................................................................................... 15 The world’s space systems Laurence NARDON .......................................................................................................... 33 Is a space weapons ban feasible? Thoughts on technology and verification of arms control in space Regina HAGEN and Jürgen SCHEFFRAN............................................................................ 41 Security without weapons in space: challenges and options Rebecca JOHNSON .......................................................................................................... 53 Resources on Outer Space Security compiled by Jon PARIS, with assistance of Melissa MOTT and Rachel WILLIAMS ............ 67 UNIDIR Focus .......................................................................................................................
    [Show full text]
  • The Space Race Documented Through Front Pages of Newspapers from Around North America
    The News Frontier The Space Race documented through front pages of newspapers from around North America Newspapers and patches generously donated to the McAuliffe-Shepard Discovery Center by Jerrid Kenney After the end of World War II, a new battle began: the Cold War. In the mid-20th century, the United States and the Soviet Union were each trying to prove they were better than the other. Both sides wanted to show the superiority of their technology, military, and, by extension, their political systems. Starting in the late 1950s, the battlefront reached space. The United States and the Soviet Union fought to first achieve milestones in space exploration—starting in 1957 with the Soviet Union’s launch of Sputnik I, continuing through the U.S.’s landing astronauts on the Moon in 1969, and ending with a handshake in space between American astronauts and Soviet cosmonauts in 1975. Witness the fight for extraterrestrial might by reading about the United States and the Soviet Union’s major feats of the Space Race, as recorded in American and Canadian newspapers in real time. The Space Race Over Time July 15-24, 1975 February 20, 1962 May 28, 1964 The Space Race comes October 4, 1957 April 12, 1961 July 20, 1969 John Glenn becomes NASA launches to an end with the Soviet Union Yuri Gagarin Neil Armstrong first American to unmanned Saturn I Apollo-Soyuz Test launches first becomes first becomes the first orbit the Earth rocket as first step Project, the in-orbit artificial satellite human in space human to walk on of the Apollo the Moon docking of U.S.
    [Show full text]
  • Space Resources for Teachers: Biology, Including Suggestions for Classroom Activities and Laboratory Experiments
    DOCUMENT RICSUMS ED 028 941 SE 006 548 By-Lee, Tom E.; And Others Space Resources for Teachers: Biology, Including Suggestions for Classroom Activities and Laboratory Experiments. California Univ., Berkeley. Spons Agency-National Aeronautics and Space Administration, Washington, D.C. Pub Date Jan 69 Note-231p. Available from-Government Printing Office, Washington, D.C. 20402 (S2.75) EDRS Price MF -S1.00 HC-S11.65 Descriptors-*AerospaceTechnology,AudiovisualAids,Bibliographies,Biology,Instruction, Laboratory Experiments, Resource Materials, Resource Units, Science Activities, Science Units,Secondary School Science Identifiers-National Aeronautics and Space Administration This compilation of resource units concerns the latest developments in space biology. Some of the topics included are oxygen consumption, temperature, radiation. rhythms, weightlessness, acceleration and vibration stress, toxicity, and sensory and perceptual problems. Many of the topics are interdisciplinary and relate biology. physiology, physics, and chemistry. Discussions of each topic include introductory paragraphs of background information, laboratory and class activities, study and discussion topics, and a useful bibliography. The studies and experiments suggested are directed at more than one student achievementlevel. Appendixed aids to the teacher indude (1) source lists of aerospace literature and research reports, (2) an annotated listing of pertinent films, and (3) lists of additional audiovisual resources. (DS) wok U.S. DEPARTMENT OF HEALTH, EDUCATION & WELFARE
    [Show full text]
  • Feasibility Study for Multiply Reusable Space Launch System
    Feasibility Study For Multiply Reusable Space Launch System. Mikhail V. Shubov University of MA Lowell One University Ave, Lowell, MA 01854 E-mail: [email protected] Contents 1 Introduction 3 2 State of Art and Proposed Orbital Delivery Systems 5 2.1 HistoricalLaunchCosts. ..... 5 2.2 LaunchCostReduction . .. .. .. .. .. .. .. ... 6 2.3 SingleStagetoOrbit(SSTO)Concept . ....... 7 2.4 Non-RocketSpaceLaunch . ... 7 3 Multiply Reusable Launch System – Purpose and Concept 9 3.1 EarlyStagesofSolarSystemColonization . .......... 9 3.2 The Concept of Multiply Reusable Launch System Consistingof MPDS and MPTO 10 4 Rocket Motion and Propulsion 11 4.1 RocketFlightPhysics.. .. .. .. .. .. .. .. .... 11 4.1.1 RocketMotion ................................ 12 4.1.2 Lossesof v ................................. 15 △ 4.2 LiquidRocketEngines ............................. ... 16 4.2.1 Enginespecifications . .. 16 4.2.2 Combustionchambertemperature . .... 17 4.3 LiquidRocketFuelsandOxidizers . ....... 18 arXiv:2107.13513v1 [physics.soc-ph] 19 Apr 2021 4.3.1 CryogenicPropellantforMPDSEngines . ..... 18 4.3.2 HypergolicPropellantforMPTOEngines . ...... 19 4.4 PropellantCost .................................. .. 21 4.4.1 MPDSPropellant–$188PerTonAverage. .... 21 4.4.2 MPTOPropellant–$2,000PerTonAverage . .... 23 1 4.4.3 OrbitalLaunchFuelBill . .. 24 5 Rocket Parameters and Performance 25 5.1 MidpointDeliverySystem(MPDS) . ..... 25 5.1.1 MainparametersofMPDSstages . .. 26 5.1.2 PerformanceandtimetableofMPDSstages . ...... 27 5.2 MidpointtoOrbitDeliverySystem(MPTO)
    [Show full text]
  • Gives an Overview of the Aerospace Industry, Its Products, Hardware
    . DOCUMENT RESUME ED 026 273 SE 006 268 By-Feirer, John L. Space Resources for the High School Industrial Arts Resource Units. Spons Agency-National Aeronautics and Space Administration, Washington, D.C. Report No-EP-44 Pub Date Apr 67 Note- 1 74p. EDRS Price MF-$0.75 HC-$8.80 Descriptors-*Aerospace Technology, Bibliographies, earth Science,Films,*IndustrialArts,Instructional i Materials, *Secondary School Science, *Teaching Guides Identifiers-National Aeronautics and Space Administration This guide is intended for industrial arts teachers, supervisors, and teacher educators at all levels of instruction for use as a supplement to their courses. The eight units which are included are all directly applicable to aerospace technology. The primary purpose of the guide is to motivate and interest students and teachers in aerospace age education. The booklet is comprised of four sections. Section One gives an overview of the aerospace industry,itsproducts, hardware, and occupations. Section Two contains eight units of student activities related to aerospace applications. Section Three is entitled "Newer Directions." Section Four is an appendix of educational services offered by the National Aeronautics and Space Administration, filmlists, and a lisst of participants ata space technology conference. (BC) r , -e-1, -.?,-. 4 :,..,0 qpprignH Gamos. LTIEN SUACCIL indunlai arts resource units Prepared for the National Aeronautics and Space Administration by a committee of industrial uts educators under the direction of John L. Feirer, Western Michigan University, in connection with a conference conducted by the University of South Florida, with the cooperation of the Florida State Department of Education and NASA's Jo Im F.
    [Show full text]
  • Mass Beam Propulsion, an Overview
    See discussions, stats, and author profiles for this publication at: https://www.researchgate.net/publication/303682465 Mass beam propulsion, an overview Article · January 2015 CITATIONS READS 0 260 2 authors, including: Adam Crowl Icarus Interstellar 22 PUBLICATIONS 22 CITATIONS SEE PROFILE Some of the authors of this publication are also working on these related projects: Galactic Surveys View project BFR to Titan View project All content following this page was uploaded by Adam Crowl on 21 August 2018. The user has requested enhancement of the downloaded file. Mass BeamJBIS, Propulsion, Vol. 68, Anpp.?-?, Overview 2015 MASS BEAM PROPULSION, AN OVERVIEW GERALD D. NORDLEY1 AND ADAM JAMES CROWL2 1. 1238 Prescott Avenue, Sunnyvale, CA 94089, USA. 2. 4 Ulmarra Crescent, Strathpine 4500, Queensland, Australia Email: [email protected] An alternative to rockets is to push spacecraft with a reflected beam. The advantage is that it leaves most of the propulsion system mass at rest. Use of mass beams, as opposed to photons, allows great efficiency by adjusting the beam velocity so the reflected mass is left near zero velocity relative to the source. There is no intrinsic limit to the proper frame map velocity that can be achieved. To make a propulsion system, subsystems need to be developed to acquire propulsive energy, accelerate the mass into a collimated beam, insure that the mass reaches the spacecraft and reflect the mass. A number of approaches to these requirements have been proposed and are summarized here. Generally no new scientific discoveries or breakthroughs are needed. These concepts are supported by ongoing progress in robotics, in nanometre scale technologies and in those technologies needed to use of space resources for the automated manufacture of space-based solar power facilities.
    [Show full text]
  • Film Catalog. John F. Kennedy Space Center. 1987. INSTITUTION National Aeronautics and Space Administration, Washington, D.C
    DOCUMENT RESUME ED 300 277 SE 050 129 TITLE Film Catalog. John F. Kennedy Space Center. 1987. INSTITUTION National Aeronautics and Space Administration, Washington, D.C. PUB DATE 87 NOTE 108p.; Photographs and some small print may not reproduce well. PUB TYPE Reference Materials - Directories/Catalogs (132) EDRS PRICE MF01/PC05 Plus Postage. DESCRIPTORS *Aerospace Education; *Aerospace Technology; Astronomy; Earth Science; Elementary School Science; Elementary Secondary Education; *Film Libraries; *Films; Instructional Materials; Satellites (Aerospace); Science Education; Science History; *Secondary School Science; Space Exploration; Space Sciences; Teaching Guides; Teaching Methods IDENTIFIERS *National Aeronautics and,tSpace Administration ABSTRACT Teachers from the United States and several other countries have access to the film library system of the National Aeronautics and Space Administration (NASA). This catalog contains the titles and abstracts for over 150 fi]ms that are available from NASA on topics regarding space flight, meteorology, astronomy, NASA programs, satellites, research, safety, technology, and earth sciences. Ordering and usage information are also included. A lesson guide is provided in the appendix to accompany 37 of these films. Each guide lists objectives, important vocabulary, preparatory activities, follow up activities, evaluation ideas, related information sources, and ideas for presenting the lesson. (CW) ******** ******** ************* ******* *** ********************** * ****** *** * Reproductions supplied by EDRS are the best that can be made * * from the original document. * f National Aeronautics. and Space Administration U.S. DEPARTMENT (Mice of Educational OF EDUCATION Research and Improvement E VCATIONAL RESOURCES INFORMATION / CENTER (ERIC) his document hasbeen reproduced eceived from the person as 4originating st. or organization O Minor changes have reoroduction Qualitybeen made to improve Points of view°, opinions meet do not necessanlystared in this claw OEM position or poky.represent official Film Catalog John F.
    [Show full text]