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Reports by Keyword(s)SPACE TO SPACE
Total Results: 18 Results per page:
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An Optoelectronics Research Center 08 MAR 2006 96 pages
Authors:  S. R. Brueck; NEW MEXICO UNIV ALBUQUERQUE
The full text of this report is available for sale.The research description contains 5 tasks divided into two general areas The first area is the area of nanomatenals and nanophotonics Two tasks are described there, the first being to understand and develop applications for a new class of nanostructured thin films, the second exploring circumstances in which metal films can transmit a high fraction of an incident electromagnetic wave. The second area of research is in new optoelectronic materials. ...


Weaponization of Space: Understanding Strategic and Technological Inevitabilities JAN 1999 38 pages
Authors:  Thomas D. Bell; AIR WAR COLL MAXWELL AFB AL
The full text of this report is available for sale.It is inevitable that humankind will weaponize space and equally likely that this will take place in the next 30 years. The United States is in the early stages of a transition from using space assets to support combat operations on the surface of the earth to using space assets to conduct combat operations in space, from space, and through space. This paper discusses factors driving the United States to ...


Performance of The TDRSS Space Deployable Antenna, FEB 1992
Authors:  Michael J. Lynch; HARRIS CORP MELBOURNE FL GOVERNMENT AEROSPACE SYSTEMS DIV
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.Satellite communication applications are continuously searching for ways to either reduce earth terminal antenna size or increase the data rate of the communication link. The Tracking and Data Relay Satellite System (TDRSS) space deployable mesh antennas provide an alternative for increased satellite antenna gain. The TDRSS space-to-space link uses a 4.8 meter diameter deployable mesh antenna. Harris Corporation delivered two deployable antennas for each of the six TDRSS satellites built ...


Space Weapons and International Law 29 MAR 1990 50 pages
Authors:  Steven J. Sloboda; NATIONAL WAR COLL WASHINGTON DC
The full text of this report is available for sale.Today's space law environment consists of a number of general positions. The United States believes in space use by all states for peaceful purposes and supports laws that will not hinder national security or peaceful progress. Defensive, nonaggressive military activity is not precluded. To the Soviet Union, space is an extension of the terrestrial environment, subject to the same political and military realities associated with the continuing struggle between capitalism ...


Analysis of Electric Propulsion Orbit Transfer Vehicles vs IUS, CENTAUR- G, and a Reuseable Bipropellant System DEC 1983
Authors:  L. W. Maddox; AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.A flexible method was developed to optimize electric orbit transfer vehicles (EOTVs) and compare them with baseline chemical systems. EOTVs have been characterized by the thruster technology and the propellant mass versus power supply mass for standardized NASA BIMOD configurations. Baseline chemical systems are represented by the Inertial Upper Stage CENTAUR-G, and a proposed reuseable LOX-LH Centaur derivative. Five electrostatic propulsion thrusters were chosen for optimization. These were the baseline ...


Modifications to Fotonap. JUL 1977
Authors:  George E. Morduch; OLD DOMINION SYSTEMS INC GAITHERSBURG MD
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.The Fotonap program has been modified (i) to include the option to compute the desired solution without inverting the normal equations matrix (thus not obtaining the solution covariance matrix), and (ii) to include the capability to handle Geoceiver measurements. For a typical run involving photogrammetric data, implementation of item (i) reduced the time taken to obtain the normal equations solution from 1 hour 50 minutes to 20 minutes. Two types ...


Satellite-to-Satellite Data Transfer and Control. 19 JAN 1977
Authors:  David M. Snider; David B. Coomber; MASSACHUSETTS INST OF TECH LEXINGTON LINCOLN LAB
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.The LES-8 and -9 satellites are three-axis stabilized earth-orbit spacecraft which provide communications at UHF and K-band frequencies with the capability of simultaneously establishing and automatically maintaining a K-band (36-38 GHz) satellite-to-satellite data link. The inter-satellite data crosslink extends the earth coverage over that which a single satellite can provide and demonstrates how a global communications system might be realized without the restrictions imposed by ground relay. This report describes ...


Recovery of Mean Gravity Anomalies From Satellite-Satellite Range Rate Data Using Least Squares Collocation. SEP 1976
Authors:  Reiner Rummel; D. P. Hajela; Richard H. Rapp; OHIO STATE UNIV COLUMBUS DEPT OF GEODETIC SCIENCE
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.Range rate data between two satellites can be used to determine acceleration along the connecting line between two satellites by numerically differentiating an analytic representation of this data. Using a reference potential field this acceleration can be interpreted to be a derivative of the disturbing potential along the line of the satellites. Using geometric techniques, the radial component of the disturbing potential can be estimated. This component can then be ...


Orbit-to-Orbit Shuttle Engine Design Study. Book 1. Parametric Cycle Study. MAY 1972
Authors:  Werner P. Luscher; AEROJET LIQUID ROCKET CO SACRAMENTO CA
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.This report presents the analytical design of propulsion systems utilizing LOX/Hydrogen propellants to be used as the propulsion for the Orbit to Orbit Space Vehicle of 65,000 lb lift-off weight. The report contains the evaluation of various engine cycles in the thrust range of 8,000 lb to 50,000 lb thrust for performance, weight and envelope culminating in the cycle selection and detail design of a 25,000 lb and 10,000 lb ...


MILLIMETER-WAVE PROPAGATION AND SYSTEMS CONSIDERATIONS OCT 1968 103 pages
Authors:  L. A. Hoffman; AEROSPACE CORP EL SEGUNDO CA LAB OPERATIONS
The full text of this report is available for sale.Applications for millimeter waves are discussed, and it is shown how propagation effects enter into systems considerations for the EHF region. The state of the millimeter-wave art is reviewed as to antennas, sources, amplifiers, and receivers. Highlighted are two applications, a high-resolution radar, which it is hoped can utilize the inherent advantage of the short millimeter wavelengths for resolution, and a space-to-space communication system at EHF.


TELEVISION TRANSMISSIONS FROM OUTER SPACE, 14 DEC 1967
Authors:  G. B. Bogatov; FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.The book tells about use of television equipment during manned space flights and about what role television will play in the organization of extraterrestrial observatories on artificial and natural celestial bodies. There are discussed problems of transmission of radiotelevision signals over cosmic distances and prospects of using for targets of space television communication of electromagnetic oscillations of the optical range of waves, and corresponding equipment is described. The book goes ...


SATELLITE DATA REDUCTION PROCESSOR SYSTEM (SADAR), OCT 1967
Authors:  John A. Fusco; Walter J. Paige; ANALYSIS AND COMPUTER SYSTEMS INC BURLINGTON MASS
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.This report describes the analysis, design and programming tasks necessary to develop a data processing and analytical programming system capable of processing information from a broad class of rockets and satellites launched as part of the AFCRL research and development mission. The Satellite Data Reduction Processor System (SADAR) described in this report is a programming system capable of processing recorded data from spacecraft with minimum change from vehicle to vehicle. ...


TRAINING ON THE PLATE. 07 JUN 1966
Authors:  Georg Maack; FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.


INVESTIGATION OF SPACE COMMUNICATIONS SYSTEMS USING LASERS. JAN 1966
Authors:  R. A. Rollin Jr.; F. Zwas; MICHIGAN UNIV ANN ARBOR INST OF SCIENCE AND TECHNOLOGY
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.Space-to-space and earth-to-space communications systems with currently available laser sources have been studied and analyzed. Conclusions are drawn concerning the best continuous wave (CW) laser wavelength for both types of systems under various conditions, and areas of research are recommended. The general optical-communications range equation was derived using signal to noise considerations for the space-to-space and earth-to-space systems. The performance of seven laser systems employing state of the art components ...


OPTIMIZATION OF FREQUENCIES FOR LOW-ALTITUDE SPACE COMMUNICATION, DEC 1964
Authors:  Gaspar R. Valenzuela; JOHNS HOPKINS UNIV LAUREL MD APPLIED PHYSICS LAB
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.A simple technique is presented for obtaining the optimum frequencies for communication with a low-altitude satellite, no higher than 800 nautical miles. The output signal-to-noise ratio at the receiving station is expressed in terms of as many parameters as possible with their respective frequency dependence. The optimum frequency is obtained by a maximization process. In cases where the exact frequency behavior of the process is too complex, an approximate analytical ...


APPLICABILITY OF LASER TECHNIQUES, 13 MAR 1964
Authors:  W. S. Litchman; ITT COMMUNICATION SYSTEMS INC PARAMUS N J
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.Laser communication techniques are presented that can be integrated into the AIRCOM System to satisfy unmet current and estimated future AF requirements. The advent of the laser has aroused great interest among communication engineers because it affords use of a new spectrum millions of megacycles wide. Although the laser will have a great impact in certain areas of communications technology, its potential in any specific area must be carefully evaluated. ...


A STUDY OF AN ORBITAL MAINTENANCE AND MATERIAL TRANSFER SHUTTLE. MAR 1964
Authors:  Ray Goodall; LOCKHEED AIRCRAFT CORP BURBANK CALIF
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.A conceptual study of an orbital maintenance and material transfer shuttle is presented. The shuttle is a one-man vehicle used for transporting personnel and materials between other orbiting vehicles and for performing maintenance and repair on space stations or unmanned satellites. The application of the shuttle to existing and proposed space systems is examined and found to be feasible and economically advantageous. The trade-offs between range, duration, propulsion and on-board ...


COMMUNICATIONS IN SPACE OPERATIONS, 24 FEB 1958
Authors:  C. M. Crain; R. T. Gabler; RAND CORP SANTA MONICA CALIF
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.The purpose of this paper is to explore the many practical factors involved in earth-space vehicle communication problem, to indicate the factors which will influence most strongly the system designs, and to point out areas in which research and development appear needed.


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