A design for a reusable water-based spacecraft known as the spacecoach. ([2016])
- Record Type:
- Book
- Title:
- A design for a reusable water-based spacecraft known as the spacecoach. ([2016])
- Main Title:
- A design for a reusable water-based spacecraft known as the spacecoach
- Further Information:
- Note: Brian McConnell, Alexander Tolley.
- Authors:
- McConnell, Brian
Tolley, Alexander - Other Names:
- International Space University.
- Contents:
- 1 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. Combining 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. Solar 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 and1 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. Combining 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. Solar 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. Development 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. Crew 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. … (more)
- Publisher Details:
- Cham [Switzerland] : Springer
- Publication Date:
- 2016
- Extent:
- 1 online resource
- Subjects:
- 629.441
Engineering
Reusable space vehicles
TECHNOLOGY & ENGINEERING -- Engineering (General)
Reusable space vehicles
Engineering
Aerospace Technology and Astronautics
Extraterrestrial Physics, Space Sciences
Science -- Astrophysics & Space Science
Astronautics
Astronautics
Astrophysics
Technology & Engineering -- Aeronautics & Astronautics
Aerospace & aviation technology
Electronic books - Languages:
- English
- ISBNs:
- 9783319226774
3319226770 - Related ISBNs:
- 9783319226767
3319226762 - Notes:
- Note: Includes bibliographical references and index.
Note: Vendor-supplied metadata. - Access Rights:
- Legal Deposit; Only available on premises controlled by the deposit library and to one user at any one time; The Legal Deposit Libraries (Non-Print Works) Regulations (UK).
- Access Usage:
- Restricted: Printing from this resource is governed by The Legal Deposit Libraries (Non-Print Works) Regulations (UK) and UK copyright law currently in force.
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library HMNTS - ELD.DS.362327
- Ingest File:
- 01_330.xml