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Prospects for the Future Development of China's Space Transportation System
2021
Space Science & Technology
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At present, the world has developed to a new stage of large-scale access to space, which has put forward higher requirements for the development of space transportation. ...
Facing the historical mission of building a space power, focusing on the construction of the China's space transportation system, this paper studied the development situation of the space transportation ...
Several commercial companies have launched new launch vehicles for the commercial market and become a new growth point for the future development of space transportation systems [8]. ...
doi:10.34133/2021/9769856
doaj:43d031a642f64582820a861552161206
fatcat:lehszkwjlraytnlfbhj4tvrg7q
Subject Index
2012
Journal of Spacecraft and Rockets
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Vehicle
412-079 Multispecies Effects for Plume Model- ing on Launch Vehicle Systems
412-085 New Method with Application to Launch Vehicle
Aerodynamic Data Dispersion
Design
A12-062 Error Estimates of the ...
A12-085 New Aerodynamic Data Dispersion Method with Application to Launch Vehicle Design
A12-087 Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel
Uninhabited and Unmanned Air Vehicles A12 ...
doi:10.2514/1.60950
fatcat:chv6alad6jglvgxm7qkxwfzrea
Spacecraft launching technique and systems
2016
2016 International Conference on Electrical, Electronics, and Optimization Techniques (ICEEOT)
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Satellites are also designed to be compatible with more then one model of launch vehicle and launching type. ...
The launch of the satellite and controlling support services are a very critical point in the creation of space-based communication technology and the most expensive phase of the total system cost. ...
The newly formed Sea Launch system is owned by the Sea Launch Partnership Limited in collaboration with four international partners such as US Boeing Commercial Space Company for designing and manufacturing ...
doi:10.1109/iceeot.2016.7755572
fatcat:f5ah5oa6qbfhhgidcx35mcmmye
New Methods for Rapid Architecture Selection and Conceptual Design
2004
Journal of Spacecraft and Rockets
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This new prior distribution then represents the best estimate of the future frequency of launch success for a new vehicle before the results of any launch attempt are known, assuming that the new vehicle ...
., “An Analysis Method for Conceptual Design of Com- plexity and Autonomy in Complex Space System Architectures,” M.S. ...
doi:10.2514/1.9203
fatcat:g4wnuigq3bbuva5wknhib5egbe
Recovered Transient Load Analysis for Payload Structural Systems
1981
Journal of Spacecraft and Rockets
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The structural system for a space mission consists of a payload integrated into a launch vehicle. ...
Basically, the method will first obtain the eigendata for an unloaded launch vehicle by removing payload A from the composite system (1). ...
doi:10.2514/3.57830
fatcat:4u3fdmnfena7bm3cx36gpvlshe
Multidisciplinary Conceptual Design Optimization of Space Transportation Systems
1999
Journal of Aircraft
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modeling and in optimization methods and frameworks for space transportation systems conceptual design and analysis. ...
of future launch vehicles will continue to be small, on the order of tens rather than hundreds, for the next decade or two while new industries develop around the decreasing costs of space launch. ...
doi:10.2514/2.2428
fatcat:ofndy4boi5h3xbfieatxndgl7a
Page 58 of American Society of Civil Engineers. Collected Journals Vol. 10, Issue AS2
[page]
1997
American Society of Civil Engineers. Collected Journals
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To take the revolutionary path, rather than the evolutionary path, to the design of space-launch vehicles will take courage. ...
The creation of mass markets for space launch services re- quires new customers with new missions, such as space tour- ism, space business parks, and large constellations of com- munications satellites ...
Parallel-burn options for dual-fuel single-stage orbital transports
1978
Journal of Spacecraft and Rockets
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Introduction
SPACE mission often utilizes an existing launch vehicle
for a new payload designed for a specific mission; such will be the case for future Shuttle missions. ...
Approach In the present investigation, a method to obtain a better estimate of a new launch vehicle/payload interface response from previous flights or analysis for a system with an iden- tical launch ...
doi:10.2514/3.27996
fatcat:3wfeg2vk4bdrxgv7hlejpdunyq
Initial Sizing and Reentry Trajectory Design Methodologies for Dual-Mode-Propulsion Reusable Aerospace Vehicles
2007
Journal of Spacecraft and Rockets
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Apart from the Space Shuttle Orbiter, all current launch vehicles are expendable. A key factor in the design of future space transportation systems is reusability. ...
space vehicle design. ...
doi:10.2514/1.30613
fatcat:qlv5xpij7nesvkl5y5a5sm24hy
Intelligent Launch and Range Operations Testbed
2003
AIP Conference Proceedings
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Innovative new methods for launch controllers to plan and control the route of launch vehicles through the National Airspace System and in-space are essential to permit multiple flights from a single spaceport ...
techniques for launch vehicle and ground systems operations. ...
doi:10.1063/1.1541307
fatcat:kgxfmmbv2nggbbokutgnfqqja4
Multidisciplinary Design Optimization of Multi-Stage Launch Vehicle using Flight Phases Decomposition
2010
International Journal for Simulation and Multidisciplinary Design Optimization
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This paper presents a new MDO method to optimize the configuration of an expendable launch vehicle and describes the application of this method to the design optimization of a small liquid fueled multi-stage ...
Optimal design of launch vehicles is a complex multidisciplinary problem. ...
Acknowledgement The work presented in this paper is part of a PhD thesis cofunded by CNES and Onera. ...
doi:10.1051/ijsmdo/2010015
fatcat:preomj2dknfc3kjrzs4f4hp5uy
Preliminary study on launch vehicle design: Applications of multidisciplinary design optimization methodologies
2017
Concurrent Engineering - Research and Applications
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The design of complex systems such as launch vehicles involves different fields of expertise that are interconnected. ...
Multidisciplinary Design Optimization (MDO) methodologies is a collection of engineering methodologies to optimize systems modeled as a set of coupled disciplinary analyses and is a key enabler to extend ...
In section 2, both classical and dedicated deterministic MDO methods for launch vehicle design are explored. ...
doi:10.1177/1063293x17737131
fatcat:3wc4ig35cbc7jpc7fkffcewmum
Opening Access to Space by Maximizing Utilization of 3D Printing in Launch Vehicle Design and Production
2020
Applied Science and Engineering Progress
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later metal additive manufacturing was widely recognized for use in propulsion systems in spacecraft and launch vehicles. ...
By optimizing launch vehicle design and production around 3D printing, the flexibility of the vehicle design, lead time, and cost of launch can be optimized to offer not just a lower cost per kilogram, ...
doi:10.14416/j.asep.2020.12.002
fatcat:mapgtyzxbnaarcw7jghdryueja
Estimation of Payload Loads Using Rigid-Body Interface Accelerations
1979
Journal of Spacecraft and Rockets
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to solve a new launch vehicle/elastic payload composite model similar to Eq. (5). ...
In the design/analysis process of a payload structural system, the accelerations at the payload/launch vehicle interface obtained from a system analysis using a rigid payload are often used as the input ...
doi:10.2514/3.57622
fatcat:clwj5ql7m5gylllv6waeykdkia
Operational considerations and comparisons of the Saturn, Space Shuttle and Ares launch vehicles
2009
2009 IEEE Aerospace conference
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This paper will identify important factors in launch vehicle design that affect the operability and availability of the system. ...
A deliberate effort is being made to ensure a high level of operability in order to significantly increase safety and availability as well as reduce recurring costs of this new launch vehicle. ...
. The astronauts who live and work in space and risk their lives every day to contribute to the success of space exploration for all mankind; The NASA engineers, scientists and support staff who commit ...
doi:10.1109/aero.2009.4839547
fatcat:vuknbb65vbek5g7fkk7r6a3ope
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