Development of an Internal-combustion Engine Fueled with Cryogenic Hydrogen and Oxygen

Development of an Internal-combustion Engine Fueled with Cryogenic Hydrogen and Oxygen
Author: Richard E Quigley (Jr)
Publisher:
Total Pages: 32
Release: 1967
Genre:
ISBN:

The practicability of utilizing a hydrogen-oxygen-fueled, internal-combustion engine in conjunction with low-pressure cryogenic tanks was determined through an experimental investigation conducted at the Air Force Aero Propulsion Laboratory. This experimental investigation incorporated subcritical tankage with a low-flow cryogenic pump, an internal-combustion power-generating unit, and associated control instrumentation. The development effort concentrated on the improvement of the endurance capabilities of the carbureted hydrogen-oxygen, internal-combustion engine. Specific performance data on all components tested are presented. One of the principal results of the investigation is the recommended use of subcooled liquid hydrogen in the cryogenic pumping system. However, further development effort on both the pumping system and the power generation are necessary before these components can be integrated successfully. (Author).

Liquid Hydrogen

Liquid Hydrogen
Author: Walter Peschka
Publisher: Springer Science & Business Media
Total Pages: 308
Release: 2012-12-06
Genre: Science
ISBN: 3709191262

to the German Edition This book is based on published material, oral presentations and lecture courses, as well as the author's personal research in the specific field of space technology and in the general areas of energy storage and transfer, and cryogenics. The science and technology of liquid hydrogen-once essential prere quisites for the rapid development of space technology-are now also proving to be more and more important for the energy production of the future. Hydrogen as an energy carrier can generally mediate the existing disparity between nuclear energy and regenerative energy, both of which are indispensable for the future. Hydrogen, as a secondary energy carrier, can be produced from these primary energy sources with minimal environmental impact and without the detrimental, long-term pollution effects of current fossil fuel technology. Hydrogen, therefore, represents the ultimate in energy technology. The initial, large-scale application of hydrogen as a secondary energy was as a high-energy rocket propellant. The procedures for its large scale liquefaction, storage and employment were generally developed in the U.S. Currently in Europe similar activities are being conducted only in France. The effort in West Germany involves testing hydrogen-oxygen and hydrogen-fluorine rocket engines, studying also the physical and technical characteristics of slush hydrogen-mixture of the solid and liquid phase-and is concentrating currently on R&D applications of liquid hydrogen as an alternate fuel. Similar activities are also being conducted in Japan and Canada.

Reference Concepts for a Space-based Hydrogen-oxygen Combustion, Turboalternator, Burst Power System

Reference Concepts for a Space-based Hydrogen-oxygen Combustion, Turboalternator, Burst Power System
Author:
Publisher:
Total Pages:
Release: 1990
Genre:
ISBN:

This report describes reference concepts for a hydrogen-oxygen combustion, turboalternator power system that supplies power during battle engagement to a space-based, ballistic missile defense platform. All of the concepts are open''; that is, they exhaust hydrogen or a mixture of hydrogen and water vapor into space. We considered the situation where hydrogen is presumed to be free to the power system because it is also needed to cool the platform's weapon and the situation where hydrogen is not free and its mass must be added to that of the power system. We also considered the situation where water vapor is an acceptable exhaust and the situation where it is not. The combination of these two sets of situations required four different power generation systems, and this report describes each, suggests parameter values, and estimates masses for each of the four. These reference concepts are expected to serve as a baseline'' to which other types of power systems can be compared, and they are expected to help guide technology development efforts in that they suggest parameter value ranges that will lead to optimum system designs. 7 refs., 18 figs., 5 tabs.

Power Systems for Space Flight

Power Systems for Space Flight
Author: Morris Zipkin
Publisher: Elsevier
Total Pages: 962
Release: 2012-12-02
Genre: Technology & Engineering
ISBN: 0323141927

Progress in Astronautics and Aeronautics, Volume 11: Power Systems for Space Flight covers certain major technical areas of space electric power. This book is organized into four parts encompassing 43 chapters that specifically tackle the selection of power systems; chemical power systems; solar power systems; heat transfer, storage, and rejection. The opening part examines the basic criteria governing the selection of space power systems for specific applications. These systems range from the very limited power requirements of a ballistic space test through the potential goals of life support in lunar exploration to the long-rage goal of electric power systems for vehicle propulsion. The second part presents the dynamics of chemical power systems, in which in which a high-temperature working fluid is employed, and static systems, such as the battery and fuel cell, in which reversible electrochemical processes are involved. The third part discusses the operative systems using photovoltaic cells and explores technological developments leading to advanced thermoelectric and thermionic static conversion systems and the larger conversion systems employing rotating machinery. This part also provides a series of papers on solar concentrators, requisite for obtaining the required high temperatures, as well as thermionic and dynamic solar power systems. The final part on heat transfer, storage, and rejection covers the space power system from energy source to waste-heat rejecting radiators. Several papers in this part describe the characteristics of alkali metal heat transfer and radiator surface conditioning. Finally, a series of papers on meteoroid penetration leads to discussions of specific radiator designs.

NASA Tech Brief

NASA Tech Brief
Author: United States. National Aeronautics and Space Administration. Technology Utilization Division
Publisher:
Total Pages: 718
Release: 1970
Genre:
ISBN: