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000742133 020__ $$a9783319226774$$q(electronic book)
000742133 020__ $$a3319226770$$q(electronic book)
000742133 020__ $$z9783319226767
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000742133 0247_ $$a10.1007/978-3-319-22677-4$$2doi
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000742133 049__ $$aISEA
000742133 050_4 $$aTL795.5
000742133 08204 $$a629.441$$223
000742133 1001_ $$aMcConnell, Brian,$$eauthor.
000742133 24512 $$aA design for a reusable water-based spacecraft known as the spacecoach  /$$cBrian McConnell, Alexander Tolley.
000742133 264_1 $$aCham [Switzerland] :$$bSpringer,$$c[2016]
000742133 300__ $$a1 online resource.
000742133 336__ $$atext$$btxt$$2rdacontent
000742133 337__ $$acomputer$$bc$$2rdamedia
000742133 338__ $$aonline resource$$bcr$$2rdacarrier
000742133 4901_ $$aSpringerBriefs in space development
000742133 504__ $$aIncludes bibliographical references and index.
000742133 5050_ $$a1 Introduction; Assumptions; 2 Water; Radiation Shielding; Heat Management; Life Support; Consumables; Debris Shielding; The Effect of Water on Crew Consumables; 3 Propulsion; Advantages and Disadvantages of Spacecoach Propulsion; Dead Weight to Working Mass; Safety; Fuel Efficiency; Refueling; Upgradability; The Rocket Equation; The Spacecoach Equation; Electric Engines; Resistojets; Microwave Electrothermal Engines (MET); RF Arc Jets; Electrodeless Lorentz Force Thrusters; Helicon Double Layer Thrusters; Hall Effect Thrusters; An Overview of Electric Propulsion Systems
000742133 5058_ $$aCombining Different Electric Propulsion TechnologiesCombining Chemical and Electrical Propulsion; Research and Development Pathway; Timeline; Questions and Gating Factors; 4 Power Plants; Battery-Assisted Solar Electric Propulsion (Exploiting the Oberth Effect); Questions and Gating Factors; 5 Life Support, Materials and Artificial Gravity; Oxygen Generation; Consumable Propellant; Carbon Supply Chain; Thermal Management; Carbon Dioxide Elimination; Radiation Shielding; Debris Shielding (Pykrete) ; Artificial Gravity; Questions and Gating Factors; 6 Upgradability
000742133 5058_ $$aSolar Arrays and Electrical BusElectric Engine Arrays; Life Support and Agricultural Systems; Avionics and Communications; Navigation Equipment; Habitable Modules; Perpetual Supply Chain; Upgrade Costs; Surface Launcher Reusability; 7 Landers; Low Gravity Moons (Phobos and Deimos) and Asteroids; Ceres; High Gravity Moons; Summary; 8 Safety and Autonomy; Space Debris; Electrical Power and Propulsion; Attitude Control; Oxygen Generation and Life Support; Food; Communication; 9 A Spacecoach Reference Design and Timeline; The Spacecoach Design Philosophy; The Crewed Ship; Cargo Ships; Landers
000742133 5058_ $$aDevelopment and Construction TimelineGround-Based Research (What's in the Works Now); Small Satellites (Near Future); Scaled Down Uncrewed Ship (3-5 Years); The USS Roddenberry; Mars Orbital Mission; The Fleet Grows; 10 Mission Templates and Cost Estimates; 11 Missions to the Cis-Lunar Environment, the Martian Moons, and the Asteroids; Cis-Lunar Space; Moon Mission Economics; Initial Ship Delivery to EML-2; Per Mission Supply Costs; Crew Launch and Return; Total; The Martian Moons; Martian Moons Mission Economics; Initial Ship Delivery and Amortization; Per Mission Refueling and Resupply Cost
000742133 5058_ $$aCrew Launch and ReturnTotal; Cost Reduction Strategies; Asteroid Interception and Mining; 12 Ceres and In Situ Resource Utilization; Why Ceres?; Surface Operations; Mission Economics; Initial Ship Delivery and Amortization; Per Mission Resupply Cost; Crew Launch and Return Cost; Total; In Situ Resource Utilization; Water ()for Consumables and Propulsion); Regolith (for Shielding, Propulsion and Tools); Pykrete (for Surface Construction); 13 Venus and Mercury; Venus; Mission Economics; Ship Delivery and Amortization; Per Mission Resupply Costs; Crew Launch and Return; Total; Mercury
000742133 506__ $$aAccess limited to authorized users.
000742133 520__ $$aBased on components already in existence, this manual details a reference design for an interplanetary spacecraft that is simple, durable, fully reusable and comprised mostly of water. Using such an accessible material leads to a spacecraft architecture that is radically simpler, safer and cheaper than conventional capsule based designs. If developed, the potential affordability of the design will substantially open all of the inner solar system to human exploration. A spacecraft that is comprised mostly of water will be much more like a living cell or a terrarium than a conventional rocket and capsule design. It will use water for many purposes before it is superheated in electric engines for propulsion, purposes which include radiation shielding, heat management, basic life support, crew consumption and comfort. The authors coined the term "spacecoaches" to describe them, as an allusion to the Prairie Schooners of the Old West, which were simple, rugged, and could live off the land.
000742133 588__ $$aVendor-supplied metadata.
000742133 650_0 $$aReusable space vehicles.
000742133 7001_ $$aTolley, Alexander,$$eauthor.
000742133 7102_ $$aInternational Space University.
000742133 77608 $$iPrint version:$$z3319226762$$z9783319226767$$w(OCoLC)913556877
000742133 830_0 $$aSpringerBriefs in space development.
000742133 85280 $$bebk$$hSpringerLink
000742133 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-3-319-22677-4$$zOnline Access$$91397441.1
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000742133 980__ $$aEBOOK
000742133 980__ $$aBIB
000742133 982__ $$aEbook
000742133 983__ $$aOnline
000742133 994__ $$a92$$bISE