A study of energy release in rocket propellants by a projectile impact method Final report
Rate of energy release in solid rocket propellants determined by square shock waves produced by projectile impact
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Rate of energy release in solid rocket propellants determined by square shock waves produced by projectile impact
We report medium resolution electron-impact induced emission spectra of CO for 20, 100 1nd 200 eV impact energies.
Terminal ballistics in hypervelocity impact of borosilicate glass projectiles on thin sheets
Determination of correlation between impact flash radiative properties and impacting meteoroid projectile characteristics
FORTRAN 4 program for calculating dynamic Kirchhoff deformation of structural rings subjected to fragment impact
Experimental measurement of rates of energy release in solid propellants subjected to strong shock waves from projectile impact
Hypervelocity impact experiments using light gas gun facility
f comets and asteroids on the Earth pose a real hazard, comparable in probability to other hazards which society deems worthy of concern. As such, it is prudent and reasonable to investigate and institute means for evaluation of the exact nature of the hazard and possible means of mitigating the effects of impacts, primarily by preventing their occurrence through orbital deflection. Decisions as to the hazard and possible detection and deflection programs must be made through a rational public discussion of the issues, provided with the best possible information. Unfortunately, some individuals have tended to overstate the problem either in terms of the probability of impact or the expected effects of impacts. The net result of such actions is often to undermine public confidence in those attempting to promote an informal discussion of the impact hazard. This is particularily true in a time of declining budgets for both science and defense, and increased competition for federal R&D dollars. It is thus important that the community find means of promoting responsible actions by the members of the community, and for dealing with public release of information, within the bounds of academic and individual freedom. The purpose of this abstract is to promote a discussion of these issues within the community and to invite additional suggestions for methods to improve the providing of accurate information to the public, the media, and most importantly, to decision makers.
Theoretical and experimental findings on atomic and molecular collisions
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This paper evaluates the performance of the PPC750 flight computer under a variety of typical high CPU utilization Flight Software activities.
Micrometeoroid mass, velocity, and composition from impact flash signature by spectroscopic analysis
This report describes the results of an investigation of phenomena associated with the oblique hypervelocity impact of spherical projectiles on multi-sheet aluminum structures. A model to be employed in the design of meteoroid and space debris protection systems for space structures is developed. The model consists of equations relating crater and perforation damage of a multi-sheet structure to parameters such as projectile size, impact velocity, and trajectory obliquity. The equations are obtained through a regression analysis of oblique hypervelocity impact test data. This data shows that the response of a multi-sheet structure to oblique impact is significantly different from its response to normal hypervelocity impact. It was found that obliquely incident projectiles produce ricochet debris that can severely damage panels or instrumentation located on the exterior of a space structure. Obliquity effects of high-speed impact must, therefore, be considered in the design of any structure exposed to the hazardous meteoroid and space debris environment.
We report medium-resolution (0.025 nm full width at half maximum (FWHM)) electron impact-induced emission spectra of CO for 20, 100, and 200 eV impact energies. The emission spectra correspond to the extreme ultraviolet transitions from the B (sup 1)Sigma(sup +)(0), and E (sup 1)Pi(0) vibronic states to the X (sup 1)Sigma(sup +)(0) ground state. The present measurements are carried out at 20 times higher spectral resolution (to separate the many blended components) compared to our previous measurements, which were at a spectral resolution of 0.5 nm FWHM. The emission cross sections corresponding to the B (sup 1)Sigma(sup +)(0) yields X (sup 1)Sigma(sup +)(0), C (sup 1)Sigma(sup +)(0) yields X (sup 1)Sigma(sup +)(0), and E (sup 1)Pi(0) yields X (sup 1)Sigma(sup +)(0) resonance transitions were measured. In addition, excitation functions (0-1 keV) extending well into the Born region have been measured for the strong transitions (B (sup 1)Sigma(sup +)(0) yields X (sup 1)Sigma(sup +)(0) and C (sup 1)Sigma(sup +)(0)) and oscillator strengths have been determined, using a modified Born approximation analytic fit to the measured excitation function.
This report critically reviews current knowledge about global distributions and properties of atmospheric aerosols, as they relate to aerosol impacts on climate. It assesses possible next steps aimed at substantially reducing uncertainties in aerosol radiative forcing estimates. Current measurement techniques and modeling approaches are summarized, providing context. As a part of the Synthesis and Assessment Product in the Climate Change Science Program, this assessment builds upon recent related assessments, including the Fourth Assessment Report of the Intergovernmental Panel on Climate Change (IPCC AR4, 2007) and other Climate Change Science Program reports. The objectives of this report are (1) to promote a consensus about the knowledge base for climate change decision support, and (2) to provide a synthesis and integration of the current knowledge of the climate-relevant impacts of anthropogenic aerosols for policy makers, policy analysts, and general public, both within and outside the U.S government and worldwide.
We report a high-resolution study (0.0036 nm full width at half maximum) of electron-impact-induced emission spectra of CO at 30-, 75-, and 100-eV electron-impact energies. The spectral features were acquired in optically thin conditions. At the specified resolution, attainable with our 3-m vacuum ultraviolet spectrometer, we observe rotationally resolved emission bands of CO in the extreme ultraviolet, from the vibronic states B (sup 1)sigma(sup +)(0), C (sup 1)sigma(sup+)(0), and E (sup 1)pi(0), to the ground state X (sup 1)sigma(sup +)(0). A simple model of these bands, based on the Honl-London factors and the rotational constants, is constructed and is shown to be in good agreement with the observed spectra. The predissociation yield for the E (sup 1)pi electronic state has been determined, showing that the E state has the largest predissociation cross section of CO for all singlet-state Rydberg series members. The excitation function of the [E (sup 1)pi(0) yields X (sup 1)sigma(sup +)(0)] transition, in the 0-800-eV impact energy range, is measured, permitting determination of the oscillator strength by using a modified Born approximation analytical fit.
We report a high-resolution study [0.0036 nm full width at half maximum (FWHM) of electron-impact-induced emission spectra of CO 1t 30, 75 and 100 eV electron-impact energies. The spectral features were acquired in optically thin conditions, and represent the highest resolution single-scattering emission spectrum of CO induced by electron impact yet available.
Improved gaseous oxygen impact test system development and consultative services