PERSEVERANCE: Rocketing to Mars with STEM
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Advanced Space Propulsion
ADVANCED SPACE PROPULSION Robert H. Frisbee, Ph.D. Jet Propulsion Laboratory California Institute of Technology Pasadena California Transportation Beyond 2000: Engineering Design for the Future September 26-28, 1995 693 ABSTRACT This presentation describes a number of advanced space propulsion technologies with the potential for meeting the need for dramatic reductions in the cost of access to space, and the need for new propulsion capabilities to enable bold new space exploration (and, ultimately, space exploitation) missions of the 21st century. For example, current Earth-to-orbit (e.g., low Earth orbit, LEO) launch costs are extremely high (ca. $10,000/kg); a factor 25 reduction (to ca. $400/kg) will be needed to produce the dramatic increases in space activities in both the civilian and overnment sectors identified in the Commercial Space Transportation Study (CSTS). imilarly, in the area of space exploration, all of the relatively "easy" missions (e.g., robotic flybys, inner solar system orbiters and landers; and piloted short-duration Lunar missions) have been done. Ambitious missions of the next century (e.g., robotic outer-planet orbiters/probes, landers, rovers, sample returns; and piloted long-duration Lunar and Mars missions) will require major improvements in propulsion capability. In some cases, advanced propulsion can enable a mission by making it faster or more affordable, and in some cases, by directly enabling the mission (e.g., interstellar missions). As a general rule, advanced propulsion systems are attractive because of their low operating costs (e.g., higher specific impulse, Isp) and typically show the most benefit for relatively "big" missions (i.e., missions with large payloads or &V, or a large overall mission model). -
Unit VI Superconductivity JIT Nashik Contents
Unit VI Superconductivity JIT Nashik Contents 1 Superconductivity 1 1.1 Classification ............................................. 1 1.2 Elementary properties of superconductors ............................... 2 1.2.1 Zero electrical DC resistance ................................. 2 1.2.2 Superconducting phase transition ............................... 3 1.2.3 Meissner effect ........................................ 3 1.2.4 London moment ....................................... 4 1.3 History of superconductivity ...................................... 4 1.3.1 London theory ........................................ 5 1.3.2 Conventional theories (1950s) ................................ 5 1.3.3 Further history ........................................ 5 1.4 High-temperature superconductivity .................................. 6 1.5 Applications .............................................. 6 1.6 Nobel Prizes for superconductivity .................................. 7 1.7 See also ................................................ 7 1.8 References ............................................... 8 1.9 Further reading ............................................ 10 1.10 External links ............................................. 10 2 Meissner effect 11 2.1 Explanation .............................................. 11 2.2 Perfect diamagnetism ......................................... 12 2.3 Consequences ............................................. 12 2.4 Paradigm for the Higgs mechanism .................................. 12 2.5 See also ............................................... -
Space Elevators: a Feasible Solution for Sending People and Goods Into Space More Cost Effectively
International Journal of Engineering Research and General Science Volume 3, Issue 5, September-October, 2015 ISSN 2091-2730 Space Elevators: A Feasible Solution for Sending People and Goods into Space More Cost Effectively Rupesh Aggarwal1, Pavleen Singh Bali2, Pranay Kami3, A.K. Raghav4 1Teaching Assistant, Department of Aerospace Engg. Amity University Gurgaon, Haryana, India 2Research Associate, Department of E & C Engg. Amity University Gurgaon, Haryana, India 3UG, Department of Aerospace Engg., Amity University Gurgaon, Haryana, India 4M.Tech. IISc Bangalore, Phd. IIT Delhi, Director- IR&D, Amity University Haryana, India Abstract— The Present study focuses on the fascinating concept of Space Elevators. Object of this study is to get introduced with every aspect in Designing, Working & Construction of Space Elevators. It‟s a concept in which tether is used to uplift any type of cargo or personnel from Earth surface to an orbit in space. Such invention not only becomes the new path for heavy loads to get into space but also becomes a cheap one. Also from the top of it, loads can be launch in any desired direction. By this not only the cost of the launch through rocket gets reduced but also the personnel handling this launch i.e. reduction of human error too. Perfect suitable material for such operation is Carbon Nano-tube which hundred times stronger and ten times lighter then Steel. In coming 50 years, it might be possible that many space elevators are ready to launch the spacecraft in space. Its application is not just only limited to the launching but also it can help in carrying heavy payloads to International Space Stations. -
Mars Options
Spaceflight A British Interplanetary Society Publication Mars UK boosts options space spending NASA’s Radiation Atlantis threats display Shuttle: icon of an age Vol 60 No 8 September 2017 www.bis-space.com CONTENTS Editor: Published by the British Interplanetary Society David Baker, PhD, BSc, FBIS, FRHS Sub-editor: Volume 60 No. 9 September 2017 Ann Page Production Assistant: 331-334 Living with the Legend Ben Jones Author of the seminal work on NASA’s Space Shuttle, Dennis Jenkins describes how he came to follow the programme through work and, as Spaceflight Promotion: a genuine enthusiast, create the massive three-volume history of its Gillian Norman design evolution and engineering. Spaceflight Arthur C. Clarke House, 334 An icon immortalised 27/29 South Lambeth Road, Laurence Withers recounts a visit to the Kennedy Space Center where he London, SW8 1SZ, England. missed a launch and came across the Space Shuttle Atlantis, more by Tel: +44 (0)20 7735 3160 Fax: +44 (0)20 7582 7167 mistake than by pre-planning, to impress and astound with its display of Email: [email protected] space artefacts. www.bis-space.com 336-342 Evaluating Mars Programme Designs ADVERTISING Stephen Ashworth has a particular view on Mars missions and judges a Tel: +44 (0)1424 883401 range of potential expeditionary modes to comment on the architecture Email: [email protected] being discussed by government agencies DISTRIBUTION and commercial providers alike. Spaceflight may be received worldwide by mail through membership of the British Interplanetary Society. Details including Library subscriptions are available from the above address. -
Achievable Space Elevators for Space Transportation and Starship
1991012826-321 :1 TRANSPORTATIONACHIEVABLE SPACEAND ELEVATORSTARSHIPSACCELERATFOR SP_CEION ._ Fl_t_ Dynamic_L',_rator_ N91-22162 Wright-PattersonAFB,Ohio ABSTRACT Spaceelevatorconceptslorlow-costspacelau,'x,,hea_rereviewed.Previousconceptssuffered;rein requirementsforultra-high-strengthmaterials,dynamicallyunstablesystems,orfromdangerofoollisionwith spacedeb._s.Theuseofmagneticgrain_reams,firstF_posedby BenoitLeben,solvestheseproblems. Magneticgrain_reamscansupportshortspace6!evatorsforliftingpayloadscheaplyintoEarthorbit, overcomingthematerialstrengthp_Oiemin.buildingspaceelevators.Alternatively,thestreamcouldsupport an internationaspaceportl circling__heEarthdailyt_nsofmilesabovetheequator,accessibleto adv_ncad aircraft.Marscouldbe equippedwitha similargrainstream,usingmaterialfromitsmoonsPhobosandDefines. Grain-streamarcsaboutthesuncould_ usedforfastlaunchestotheouterplanetsandforaccelerating starshipsto nearikjhtspeedforinterstella:recor_naisar',cGraie. nstreamsareessentiallyimperviousto collisions,andcouldreducethecost_f spacetranspo_ationbyan o_er c,,fmagnih_e. iNTRODUCTION Themajorob_,tacletorapi( spacedevei,apmentisthehighco_ oflaunct_!,'D_gayloadsintoEarthorbit. Currentlaunchcostsare morethan_3000per kilogramand, rocketvehicles_ch asNASP,S,_nger_,'_the AdvancedLaunchSystemwiltstillcost$500perkilogram.Theprospectsforspaceente_dseandsettlement. arenotgoodunlessthesehighlaunchc_stsarereducedsignificantly. Overthepastthirtyyears,severalconceptshavebeendevelopedforlaunchir_la{_opayloadsintoEarth orbitcheaplyusing"_rJeceelevators."The._estructurescanbesupportedbyeithe.rs_ati,for:: -
Amusementtodaycom
KINGS ISLAND’S 40th ANNIVERSARY – PAGES 19-22 TM Vol. 16 • Issue 3 JUNE 2012 Two traditional parks turn to Zamperla for thrill factor AirRace takes flight at Utah’s Lagoon Massive Black Widow swings into historic Kennywood Park FARMINGTON, Utah — Inspired by what they saw at Co- STORY: Scott Rutherford ney Island’s Luna Park last year, Lagoon officials called upon [email protected] Zamperla to create for them a version of the Italian ride manu- WEST MIFFLIN, Pa. — facturer’s spectacular AirRace attraction. Guests visiting Kennywood Just as with the proptype AirRace at Luna Park, Lagoon’s Park this season will find new ride replicates the thrill and sensations of an acrobatic air- something decidedly sinister plane flight with maneuvers such as banks, loops and dives. lurking in the back corner of Accommodating up to 24 riders in six four-seater airplane- Lost Kennywood. The park’s shaped gondolas, AirRace combines a six-rpm rotation with a newest addition to its impres- motor driven sweep undulation that provides various multi- sive ride arsenal is Black vectored sensations. The gondolas reach a maximum height of Widow, a Zamperla Giant 26 feet above the ground while ‘pilots’ feel the acceleration of Discovery 40 swinging pen- almost four Gs, both right-side-up and inverted. The over-the- dulum ride. shoulder restraint incorporated into the seats holds riders during Overlooking the the simulated flight, and with a minimum height requirement of final swoop turn of the just 48 inches, AirRace is one of Lagoon’s most accessible family Phantom’s Revenge and the thrill rides. -
Today's Space Elevator
International Space Elevator Consortium ISEC Position Paper # 2019-1 Today's Space Elevator Space Elevator Matures into the Galactic Harbour A Primer for Progress in Space Elevator Development Peter Swan, Ph.D. Michael Fitzgerald ii Today's Space Elevator Space Elevator Matures into the Galactic Harbour Peter Swan, Ph.D. Michael Fitzgerald Prepared for the International Space Elevator Consortium Chief Architect's Office Sept 2019 iii iv Today's Space Elevator Copyright © 2019 by: Peter Swan Michael Fitzgerald International Space Elevator Consortium All rights reserved, including the rights to reproduce this manuscript or portions thereof in any form. Published by Lulu.com [email protected] 978-0-359-93496-6 Cover Illustrations: Front – with permission of Galactic Harbour Association. Back – with permission of Michael Fitzgerald. Printed in the United States of America v vi Preface The Space Elevator is a Catalyst for Change! There was a moment in time that I realized the baton had changed hands - across three generations. I was talking within a small but enthusiastic group of attendees at the International Space Development Conference in June 2019. On that stage there was generation "co-inventor" Jerome Pearson, generation "advancing concept" Michael Fitzgerald and generation "excited students" James Torla and Souvik Mukherjee. The "moment" was more than an assembly of young and old. It was also a portrait of the stewards of the Space Elevator revolution -- from Inventor to Developer to Innovators. James was working a college research project on how to get to Mars in 77 days from the Apex Anchor and Souvik (16 years old) was representing his high school from India. -
System Engineering Analysis of Terraforming Mars with an Emphasis on Resource Importation Technology
LMU/LLS Theses and Dissertations 12-2018 System Engineering Analysis of Terraforming Mars with an Emphasis on Resource Importation Technology Brandon Wong Loyola Marymount University, [email protected] Follow this and additional works at: https://digitalcommons.lmu.edu/etd Part of the Systems Engineering Commons Recommended Citation Wong, Brandon, "System Engineering Analysis of Terraforming Mars with an Emphasis on Resource Importation Technology" (2018). LMU/LLS Theses and Dissertations. 888. https://digitalcommons.lmu.edu/etd/888 This Research Projects is brought to you for free and open access by Digital Commons @ Loyola Marymount University and Loyola Law School. It has been accepted for inclusion in LMU/LLS Theses and Dissertations by an authorized administrator of Digital Commons@Loyola Marymount University and Loyola Law School. For more information, please contact [email protected]. System Engineering Analysis of Terraforming Mars with an Emphasis on Resource Importation Technology Loyola Marymount University, Systems Engineering Leadership Program Capstone Project Abstract This project uses System Engineering principles to delve into the viability of different methods for Terraforming Mars, with a comparison between Paraterraforming, Terraforming and Bioforming. It will then examine one subsystem that will be integral to the terraforming process, which is the space infrastructure necessary to import enough gases to recreate Earth’s atmosphere on Mars. It will analyze the viability of Chemical Rockets, Nuclear Rockets, Space -
Magnetic Levitation Technology As a Means to Provide Launch Capability to Future Space Bound Vehicles
A University of Sussex DPhil thesis Available online via Sussex Research Online: http://sro.sussex.ac.uk/ This thesis is protected by copyright which belongs to the author. This thesis cannot be reproduced or quoted extensively from without first obtaining permission in writing from the Author The content must not be changed in any way or sold commercially in any format or medium without the formal permission of the Author When referring to this work, full bibliographic details including the author, title, awarding institution and date of the thesis must be given Please visit Sussex Research Online for more information and further details Vacuum Maglev – An international endeavour for a global space program By Tanay Sharma SUBMITTED FOR THE DEGREE OF DOCTOR OF PHILOSOPHY AT THE UNIVERSITY OF SUSSEX School of Engineering and Informatics University of Sussex Brighton April 2012 I Declaration I Tanay Sharma hereby declare that contents of this thesis have not and will not be distributed in part or in full to another University or Institution towards an award of any other degree. Signature Tanay Sharma Dated: 12 April 2012 II Summary This thesis focuses on the use of magnetic levitation technology as a means to provide launch capability to future space bound vehicles. Building on past work and after an extensive literature review, we aim to show how magnetic levitation and propulsion can be an economically and socially justifiable means to launch cargo and passengers for the purpose of reconnaissance, space tourism, and deep space exploration. Based on the validity of the technology, we look at the economic and political viability of establishing a magnetic levitation and propulsion launch system and compare it with current launch systems. -
Maglev (Transport) 1 Maglev (Transport)
Maglev (transport) 1 Maglev (transport) Maglev, or magnetic levitation, is a system of transportation that suspends, guides and propels vehicles, predominantly trains, using magnetic levitation from a very large number of magnets for lift and propulsion. This method has the potential to be faster, quieter and smoother than wheeled mass transit systems. The power needed for levitation is usually not a particularly large percentage of the overall consumption; most of the power used is needed to overcome air drag, as with any other high speed train. The highest recorded speed of a Maglev train is 581 kilometres per JR-Maglev at Yamanashi, Japan test track in hour (361 mph), achieved in Japan in 2003, 6 kilometres per hour November, 2005. 581 km/h. Guinness World (3.7 mph) faster than the conventional TGV speed record. Records authorization. The first commercial Maglev "people-mover" was officially opened in 1984 in Birmingham, England. It operated on an elevated 600-metre (2000 ft) section of monorail track between Birmingham International Airport and Birmingham International railway station, running at speeds up to 42 km/h (26 mph); the system was eventually closed in 1995 due to reliability and design problems. Perhaps the most well known implementation of high-speed maglev technology currently operating commercially is the IOS (initial operating segment) demonstration line of the German-built Transrapid Transrapid 09 at the Emsland test facility in train in Shanghai, China that transports people 30 km (18.6 miles) to Germany the airport in just 7 minutes 20 seconds, achieving a top speed of 431 km/h (268 mph), averaging 250 km/h (160 mph). -
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) -
Analysis of Levitational Systems for a Superconducting Launch Ring*
Analysis of Levitational Systems for a Superconducting Launch Ring* John R. Hull,1 James Fiske,2 Ken Ricci,2 and Michael Ricci2 1Energy Technology Division, Argonne National Laboratory, 9700 S. Cass Avenue, Argonne, IL 60439 USA 2LaunchPoint Technologies LLC, 5735-B Hollister Avenue, Goleta, CA 93317 USA May 2006 The submitted manuscript has been created by the University of Chicago as Operator of Argonne National Laboratory (“Argonne”) under Contract No. W-31-109-ENG- 38 with the U.S. Department of Energy. The U.S. Government retains for itself, and others acting on its behalf, a paid-up, nonexclusive, irrevocable worldwide license in said article to reproduce, prepare derivative works, distribute copies to the public, and perform publicly and display publicly, by or on behalf of the Government. For presentation at the 2006 Applied Superconductivity Conference, Seattle, WA, August 27- September 1, 2006. *This work was supported by the U.S. Department of Energy under Contract W-31-109-Eng-38 and by the U.S. Air Force under Contract no. FA9550-05-C-0111. Analysis of Levitational Systems for a Superconducting Launch Ring John R. Hull Energy Technology Division, Argonne National Laboratory James Fiske, Ken Ricci and Michael Ricci LaunchPoint Technologies ABSTRACT The launch ring consists of a maglev system in which a levitated vehicle is accelerated in an evacuated circular tunnel until it reaches a desired velocity and then releases a projectile into a path leading to the atmosphere. This paper analyses several levitational concepts for a system that employs superconductors in the stator and on the vehicle.