2 edition of Nuclear propulsion [and] chemical propulsion. found in the catalog.
Nuclear propulsion [and] chemical propulsion.
United States. Congress. House. Committee on Science and Astronautics.
Published
1964
by U.S. Govt. Print. Off. in Washington
.
Written in English
Classifications | |
---|---|
LC Classifications | TL795 .U5 |
The Physical Object | |
Pagination | iii, 85 p. |
Number of Pages | 85 |
ID Numbers | |
Open Library | OL5931948M |
LC Control Number | 64061403 |
OCLC/WorldCa | 10975300 |
Nuclear thermal propulsion, where a fission reactor heats propellants like hydrogen that are then accelerated through a nozzle, holds the potential of . Perigee propulsion for orbital launch of nuclear rockets / (Washington, D. C.: National Aeronautics and Space Administration ; Springfield, Va.: for sale by the Clearinghouse for Federal Scientific and Technical Information, ), by Paul G. Johnson, Frank E. Rom, and United States National Aeronautics and Space Administration (page images.
Nuclear Propulsion vs. Chemical Propulsion I would like to start of by tell the chemical side. After that i will state the nuclear side. in conclusion I will put the two together to find out with is better is terms of cost, speed, weight, fuel, and degree of safety. Chemical Propulsion: Chemical propulsion is a . Principles of Nuclear Rocket Propulsion provides an understanding of the physical principles underlying the design and operation of nuclear fission-based rocket engines. While there are numerous texts available describing rocket engine theory and nuclear reactor theory, this is the first book available describing the integration of the two.
Nuclear Propulsion, Nuclear Thermal Propulsion, Nuclear Electric Propulsion, Flight Time SECURITY CLASSIFICATION OF: LIMITATION OF ABSTRACT NUMBER OF PAGES 19a. NAME OF RESPONSIBLE PERSON C1C Michael J. Osenar a. REPORT U b. ABSTRACT N/A U c. THIS PAGE U 11 19b. TELEPHONE NUMBER (include area code) () Standard Form File Size: KB. Nuclear Propulsion Nuclear energy remains an attractive potential means of propulsion for future spacecraft. When compared with conventional rocket engines, a nuclear propulsion system would in theory be less massive, and could provide sustained thrust with greater energy. Many believe nuclear-powered spacecraft can and should be built, but first many technical problems and other hurdles must.
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In a chemical rocket, hot gases are created by chemical combustion; in a nuclear rocket heating of the propellant in a nuclear reactor creates hot gas.
In either case, the hot gases flow through the throat of the rocket nozzle where they expand and Nuclear propulsion [and] chemical propulsion.
book thrust. Extensive development effort has been expended on nuclear rockets.5/5(8). Principles of Nuclear Rocket Propulsion provides an understanding of the physical principles underlying the design and operation of nuclear fission-based rocket engines.
While there are numerous texts available describing rocket engine theory and nuclear reactor theory, this is the first book available describing the integration of the two subject by: 1. At the center of NASA’s nuclear rocket program is Bill Emrich, the man who literally wrote the book on nuclear propulsion.
“You can do chemical propulsion to Mars, but it’s really hard. Get this from a library. Nuclear propulsion [and] chemical propulsion: hearings before the Subcommittee on Science and Astronautics, U.S.
House of Representatives, Eighty-eighth Congress, second session. March 18 [United States. Congress. House. Committee on Science and Astronautics. Subcommittee on NASA Oversight.]. InNASA began an R&D effort to develop nuclear power and propulsion systems for solar system exploration.
This activity, renamed Project Prometheus inwas initiated because of the inherent limitations in photovoltaic and chemical propulsion systems in reaching many solar system objectives. Nuclear Propulsion for Rockets.
A Layman's Guide to Project Rover by Los Alamos Scientific Laboratory, University of California and a great selection of related books, art and collectibles available now at American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA ^Nuclear (NERVA) solid-core propulsion systems are compared to ad- vanced cryogenic (Fg/H.
and CL/HJ chemical propulsion systems for an orbit-to-orbit vehicle operating in the earth-moon space. The orbit-to-orbit vehicle is assumed to use propellants delivered by a reusable earth-to-orbit shuttle (EOS).
Chemical retropropulsion is used, if necessary, to decrease entry speed to this value. (5) For configuration (4), the command module and the propulsion module are cap tured at Earth return into a low circular parking orbit using nuclear propulsion. (6) The payload and stage input parameters used are based on references 29Author: E.
Willis. Principles of Nuclear Rocket Propulsion. provides an understanding of the physical principles underlying the design and operation of nuclear fission-based rocket engines.
While there are numerous texts available describing rocket engine theory and nuclear reactor theory, this is the first book available describing the integration of the two subject areas. The Fusion Driven Rocket: Nuclear Propulsion through Direct Conversion of Fusion Energy energy density gain of nuclear fuel when compared to chemical combustion energy.
Current nuclear fusion efforts have focused on the generation of electric grid power and are wholly File Size: 1MB. During the last decade, rapid growth of knowledge in the field of jet, rocket, nuclear, ion and electric propulsion has resulted in many advances useful to the student, engineer and scientist.
The purpose for offering this course is to make available to them these recent advances in theory and. It was the second-stage and airplane applic ation that drove R&D in nuclear propulsion. W i t h t h e a d v e n t o f r el ia bl e I CB M (th e A t l a s missile) and lighter fission and Author: Claudio Bruno.
Advanced cryogenic chemical propulsion systems achieve a maximum specific impulse (Isp) of about seconds. The Nuclear Engine for Rocket Vehicle Application (NERVA) program of the 's built engines with Isp's of about seconds.
Starting in the mids, the United States initiated a program to develop nuclear propulsion for spacecraft. The basic technology involved passing hydrogen through a very high temperature nuclear reactor, where it expanded and blasted out of the reactor at high velocity.
NASA is currently investigating nuclear thermal propulsion as an alternative to chemical propulsion for manned missions to the outer planets. There are a number of materials being considered for use as fuel elements. These materials include tricarbides and CERMETS such as W/UO2, Mo/UO2, W/UN and Mo/UN.
All of these materials require high temperature processing to achieve the required : Dennis S. Tucker. The Naval Nuclear Propulsion Program comprises the military and civilian personnel who design, build, operate, maintain, and manage the nuclear-powered ships and the many facilities that support the U.S.
nuclear-powered naval fleet. The Program has cradle-to-grave responsibility for all naval nuclear propulsion matters. 9 Outer Space Propulsion by Nuclear Energy, hearings before subcommittees of the Joint Committee on Atomic Energy, Congress of The United States, 85th Cong., 2nd sess., January 22 23, and February 6 10 Bussard, R.
W., and R. DeLauer. Nuclear Rocket Propulsion, McGraw-Hill. Abstract—The nuclear thermal rocket (NTR) represents the next “evolutionary step” in high performance rocket propulsion.
Unlike conventional chemical rockets that produce their energy through combustion, the NTR derives its energy from fission of Uranium atoms contained within fuel elements that comprise the engine’s reactor by: Nuclear propulsion has emerged from the doldrums and is now seen as a definite possibility for outer solar system robotic exploration; and as enabling technology for a human mars expedition.
A new chapter on nuclear thermal propulsion has been added to reflect this revival of interest. Nuclear thermal propulsion (NTP) systems have been studied in both the USA and the former Soviet Union since the s for use in space science and exploration missions.
NTP uses nuclear fission to heat hydrogen to very high temperatures in a short amount of time so that the hydrogen can provide thrust as it accelerates through an engine : Douglas Burns, Stephen Johnson.Principles of Nuclear Rocket Propulsion provides an understanding of the physical principles underlying the design and operation of nuclear fission-based rocket engines.
While there are numerous texts available describing rocket engine theory and nuclear reactor theory, this is the first book available describing the integration of the two subject areas.chemical systems. As missions aim for targets farther out into the solar system, nuclear propulsion may offer the only viable technological option for extending the reach of exploration missions beyond Mars.
Because NTP provides the fastest trip time of all currently obtainable advanced propulsion sys-File Size: 1MB.