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Displaying 1—10 of 1000 matches for query "Orbital_Refueling_Feasibility_Study_and_Design_Concept" retrieved in 0.024 sec with these stats:
- "orbit" found 23590 times in 8183 documents
- "refuel" found 223 times in 158 documents
- "feasibl" found 823 times in 716 documents
- "studi" found 10497 times in 5293 documents
- "and" found 284902 times in 19361 documents
- "design" found 11297 times in 5478 documents
- "concept" found 2924 times in 1581 documents
... Horizon studies for the Army Ballistic Missile Agency. Many of the ABMA documents were not widely disseminated because they fell outside the purview of later NASA preservation contracts.
Media:1960Orbital Refuelling.pdf Orbital Refueling Feasibility Study and Design Concept (ABMA 1960)
Media:1960Orbital_Refuelling2.pdf Orbital Refueling Feasibility Study and Design Concept Part II (ABMA 1960)
Category:Publications
... AERODYNAMICS, PROPULSION, STRUCTURES AND DESIGN PRACTICE'''
by Bonney, E. A., M. J. Zucrow, and C. W. Besserer
''Princeton (New Jersey), 1956: D. van Nostrand Co., Inc., 595 pages, $12. ... nozzles, turbojet. ramjet and rocket engines; airframe design, environmental loads, characteristics of materials, fabrication methods, reliability, packaging engineering and composite design.
Extracted from the 1962 Publication ''Annotated Bibliography of Space Science and Technology with an ...
... the feasibility of using a radioisotope thermal rocket with in-situ atmospheric CO2 propellant to deliver a 10 kg payload from the Martian surface to a 200 km circular orbit ... expansion losses to the degree that if more realistic and computationally-intensive models are incorporated, the effect will definitively disprove the concept with currently available technology. Based on this preliminary ...
... orbital dynamics, mass drivers, dispersers
'''JBIS Reference Code ''' - 2005.58.310
'''Number of Pages''' - 6
Abstract
This paper compares two non-nuclear planetary defense mitigation concepts - as well as a hybrid concept ... of the asteroid. The brief study concludes that the Disperser is preferred over the Mass Driver regarding the energy requirements, complexity and technical risk; while ...
... ''' - 368-374
'''Year''' - 2006
'''Keywords''' - Orbital tower, payload transfer, orbital dynamics
'''JBIS Reference Code ''' - 2006.59.368
'''Number of Pages''' - 7
Abstract
A new concept for propellantless payload transfer ... rotation to the escaping mass. The dynamics of the siphon effect are explored and key engineering issues are identified.
'''To BUY this paper click http://www. ...
... reviewed. Landers and balloons satisfy a limited set of scientific objectives; aeroplanes seem largely impractical due to high power requirements or structural challenges. Airships and helicopters appear to be quite feasible, given several advantageous aspects of Titan's environment, and would satisfy the broadest range of scientific objectives.
'''To ...
... design configuration and mission profile and these are discussed prior to entering Phase IV of the design study which begins the process of down selecting design options. This paper represents a progress report on Project Icarus and is a submission of the Project Icarus Study Group.
... in heliocentric orbits inclined to the ecliptic plane are to be used for exploration of the Sun and monitoring of space weather in the Earth environment. The satellites achieve the inclined orbits at ... -assisted maneuvers at the inner planets (Earth and Venus) with the aid of electric-jet engines. The orbital planes are mutually perpendicular and the satellites in orbit are spaced by a quarter of a ...
... used to maintain their position in orbit. The thrusters would only be used occasionally to maintain correct position because the module would be orbiting around Earth and the gravitational pull would keep it in place. At first, the modules will orbit around the Earth but, in the future, the modules will be docked together in space and ...
... Perspective: Who are the global participants in the commercial space business and their strengths and weaknesses. - Comprehensive Review: A wide-ranging review and assessment of the various launch systems, the ever expanding number ... nature of commercial space in terms of launch technology, safety concerns, insurance, laws and regulation, financial requirements, and marketing strategies.Image:9781894959988.jpg '''Buy This Book''' http://apogeebooks.com ...
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