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A Two-Stage-To-Orbit Spaceplane Concept with Growth Potential

A Two-Stage-To-Orbit Spaceplane Concept with Growth Potential
Author: Unmeel B. Mehta
Publisher: BiblioGov
Total Pages: 32
Release: 2013-08
Genre:
ISBN: 9781289282844

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A two-stage-to-orbit (TSTO) spaceplane concept developed in 1993 is revisited, and new information is provided to assist in the development of the next-generation space transportation vehicles. The design philosophy, TSTO spaceplane concept, and the design method are briefly described. A trade study between cold and hot structures leads to the choice of cold structures with external thermal protection systems. The optimal Mach number for staging the second stage of the TSTO spaceplane (with air-breathing propulsion on the first stage) is 10, based on life-cycle cost analysis. The performance and specification of a prototype/experimental (P/X) TSTO spaceplane with a turbo/ram/scramjet propulsion system and built-in growth potential are presented and discussed. The internal rate of return on investment is the highest for the proposed TSTO spaceplane, vis-A-vis a single-stage-to-orbit (SSTO) rocket vehicle and a TSTO spaceplane without built-in growth. Additional growth potentials for the proposed spaceplane are suggested. This spaceplane can substantially decrease access-to-space cost and risk, and increase safety and reliability in the near term It can be a serious candidate for the next-generation space transportation system.


Conceptual Design of Two-Stage-To-Orbit Hybrid Launch Vehicle

Conceptual Design of Two-Stage-To-Orbit Hybrid Launch Vehicle
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 278
Release: 2018-07-24
Genre:
ISBN: 9781723546334

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The object of this design class was to design an earth-to orbit vehicle to replace the present NASA space shuttle. The major motivations for designing a new vehicle were to reduce the cost of putting payloads into orbit and to design a vehicle that could better service the space station with a faster turn-around time. Another factor considered in the design was that near-term technology was to be used. Materials, engines and other important technologies were to be realized in the next 10 to 15 years. The first concept put forth by NASA to meet these objectives was the National Aerospace Plane (NASP). The NASP is a single-stage earth-to-orbit air-breathing vehicle. This concept ran into problems with the air-breathing engine providing enough thrust in the upper atmosphere, among other things. The solution of this design class is a two-stage-to-orbit vehicle. The first stage is air-breathing and the second stage is rocket-powered, similar to the space shuttle. The second stage is mounted on the top of the first stage in a piggy-back style. The vehicle takes off horizontally using only air-breathing engines, flies to Mach six at 100,000 feet, and launches the second stage towards its orbital path. The first stage, or booster, will weigh approximately 800,000 pounds and the second stage, or orbiter will weigh approximately 300,000 pounds. The major advantage of this design is the full recoverability of the first stage compared with the present solid rocket booster that are only partially recoverable and used only a few times. This reduces the cost as well as providing a more reliable and more readily available design for servicing the space station. The booster can fly an orbiter up, turn around, land, refuel, and be ready to launch another orbiter in a matter of hours. Unspecified Center NASA-CR-190006, NAS 1.26:190006 NASW-4435...


Spaceflight Revolution

Spaceflight Revolution
Author: David Ashford
Publisher: World Scientific
Total Pages: 204
Release: 2002-12-10
Genre: Technology & Engineering
ISBN: 1783261234

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A revolution in spaceflight is likely soon with the prospect of everyday access to orbit within fifteen years. Costly launch vehicles based on ballistic missiles will be replaced by ‘spaceplanes’, using technology that exists today. In five years' time, a prototype could be built, and with a further ten years of detailed development, the design could approach airliner maturity, reducing the cost of sending people into space some one thousand times to around US$20,000.Spaceplane development has, in effect, been suppressed by entrenched thinking and short-term vested interests. But the present monopoly of large government space agencies is becoming unsupportable, and the market that understands the very real opportunities for space travel will be reaching critical mass in the near future.This book examines these issues and shows why space tourism will one day become the single largest business in space, and how astronomy and environmental science will be transformed by low-cost access making possible instruments vastly larger than those of today.


Spaceplane

Spaceplane
Author: Fouad Sabry
Publisher: One Billion Knowledgeable
Total Pages: 451
Release: 2022-10-25
Genre: Transportation
ISBN:

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What Is Spaceplane A vehicle that is capable of flying and gliding like an airplane while in the atmosphere of Earth and maneuvering like a spacecraft while in space is referred to as a spaceplane. In order to do this, spaceplanes need to include aspects of both aviation and spacecraft into their design. Sub-orbital spaceplanes often resemble fixed-wing aircraft more than orbital spaceplanes do, whereas orbital spaceplanes tend to be more analogous to conventional spacecraft. Rockets have been used to power every spaceplane that has ever flown, but gliders have been used to land them. How You Will Benefit (I) Insights, and validations about the following topics: Chapter 1: Spaceplane Chapter 2: Human spaceflight Chapter 3: Buran programme Chapter 4: Spacecraft Chapter 5: Spaceflight Chapter 6: Lifting body Chapter 7: Human spaceflight programs Chapter 8: Reusable launch system Chapter 9: Boeing X-20 Dyna-Soar Chapter 10: Lockheed Martin X-33 Chapter 11: Boeing X-37 Chapter 12: Dream Chaser Chapter 13: Launch vehicle Chapter 14: List of crewed spacecraft Chapter 15: Intermediate eXperimental Vehicle Chapter 16: Buran (spacecraft) Chapter 17: USA-212 Chapter 18: Takeoff and landing Chapter 19: XS-1 (spacecraft) Chapter 20: Space Rider Chapter 21: SNC Demo-1 (II) Answering the public top questions about spaceplane. (III) Real world examples for the usage of spaceplane in many fields. (IV) 17 appendices to explain, briefly, 266 emerging technologies in each industry to have 360-degree full understanding of spaceplane' technologies. Who This Book Is For Professionals, undergraduate and graduate students, enthusiasts, hobbyists, and those who want to go beyond basic knowledge or information for any kind of spaceplane.


Technology Roadmap for Dual-Mode Scramjet Propulsion to Support Space-Access Vision Vehicle Development

Technology Roadmap for Dual-Mode Scramjet Propulsion to Support Space-Access Vision Vehicle Development
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 28
Release: 2018-06-20
Genre:
ISBN: 9781721532681

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Third-generation reusable launch vehicle (RLV) systems are envisioned that utilize airbreathing and combined-cycle propulsion to take advantage of potential performance benefits over conventional rocket propulsion and address goals of reducing the cost and enhancing the safety of systems to reach earth orbit. The dual-mode scramjet (DMSJ) forms the core of combined-cycle or combination-cycle propulsion systems for single-stage-to-orbit (SSTO) vehicles and provides most of the orbital ascent energy. These concepts are also relevant to two-stage-to-orbit (TSTO) systems with an airbreathing first or second stage. Foundation technology investments in scramjet propulsion are driven by the goal to develop efficient Mach 3-15 concepts with sufficient performance and operability to meet operational system goals. A brief historical review of NASA scramjet development is presented along with a summary of current technology efforts and a proposed roadmap. The technology addresses hydrogen-fueled combustor development, hypervelocity scramjets, multi-speed flowpath performance and operability, propulsion-airframe integration, and analysis and diagnostic tools. Cockrell, Charles E., Jr. and Auslender, Aaron H. and Guy, R. Wayne and McClinton, Charles R. and Welch, Sharon S. Langley Research Center AIAA Paper 2002-5188


The Scramjet Engine

The Scramjet Engine
Author: Corin Segal
Publisher: Cambridge University Press
Total Pages: 271
Release: 2009-06-22
Genre: Technology & Engineering
ISBN: 0521838150

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Demand for high-speed propulsion has renewed development of the supersonic combustion ramjet engine (Scramjet engine) for hypersonic flight applications.


The Space Shuttle Decision

The Space Shuttle Decision
Author: T. A. Heppenheimer
Publisher:
Total Pages: 0
Release: 1999
Genre: Space shuttles
ISBN:

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Long before the NASA was the throes of planning for the Apollo voyages to the Moon, many people had seen the need for a vehicle that could access space routinely. The idea of a reusable space shuttle dates at least to the theoretical rocketplane studies of the 1930s, but by the 1950s it had become an integral part of a master plan for space exploration. The goal of efficient access to space in a heavy-lift booster prompted NASA's commitment to the space shuttle as the vehicle to continue human space flight. By the mid-1960s, NASA engineers concluded that the necessary technology was within reach to enable the creation of a reusable winged space vehicle that could haul scientific and applications satellites of all types into orbit for all users. President Richard M. Nixon approved the effort to build the shuttle in 1972 and the first orbital flight took place in 1981. Although the development program was risky, a talented group of scientists and engineers worked to create this unique space vehicle and their efforts were largely successful. Since 1981, the various orbiters -Atlantis, Columbia, Discovery, Endeavour, and Challenger (lost in 1986 during the only Space Shuttle accident)- have made early 100 flights into space. Through 1998, the space shuttle has carried more than 800 major scientific and technological payloads into orbit and its astronaut crews have conducted more than 50 extravehicular activities, including repairing satellites and the initial building of the International Space Station. The shuttle remains the only vehicle in the world with the dual ability to deliver and return large payloads to and from orbit, and is also the world's most reliable launch system. The design, now almost three decades old, is still state-of-the-art in many areas, including computerized flight control, airframe design, electrical power systems, thermal protection system, and main engines. This significant new study of the decision to build the space shuttle explains the shuttle's origin and early development. In addition to internal NASA discussions, this work details the debates in the late 1960s and early 1970s among policymakers in Congress, the Air Force, and the Office of Management and Budget over the roles and technical designs of the shuttle. Examining the interplay of these organizations with sometimes conflicting goals, the author not only explains how the world's premier space launch vehicle came into being, but also how politics can interact with science, technology, national security, and economics in national government.