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Transonic wind tunnel tests of the launch, jettison, and longitudinal characteristics of an airplane and missile model combination

Description: Report presenting tests of an airplane model equipped with missiles to investigate the capability of that combination to achieve satisfactory launching and jettisoning of the missiles. Information about pylon modifications, missiles in launch positions, missile trajectory, and missiles in jettison positions is provided.
Date: November 20, 1957
Creator: Cleary, Joseph W.; Frank, Joseph L. & Dewey, C. Forbes, Jr.
Partner: UNT Libraries Government Documents Department

Preliminary Evaluation of the Wing Leading Edge as a Missile-Mounting Location

Description: Report discussing testing to evaluate some of the major aspects of mounting and launching missiles from the leading edge of a wing, including experimentation with six missile models at several Mach numbers. Information from flight tests and launching tests is provided.
Date: January 16, 1957
Creator: Hill, P. R. & Hoffman, S.
Partner: UNT Libraries Government Documents Department

Towards a standards-compliant genomic and metagenomic publication record

Description: Increasingly we are aware as a community of the growing need to manage the avalanche of genomic and metagenomic data, in addition to related data types like ribosomal RNA and barcode sequences, in a way that tightly integrates contextual data with traditional literature in a machine-readable way. It is for this reason that the Genomic Standards Consortium (GSC) formed in 2005. Here we suggest that we move beyond the development of standards and tackle standards-compliance and improved data capture at the level of the scientific publication. We are supported in this goal by the fact that the scientific community is in the midst of a publishing revolution. This revolution is marked by a growing shift away from a traditional dichotomy between 'journal articles' and 'database entries' and an increasing adoption of hybrid models of collecting and disseminating scientific information. With respect to genomes and metagenomes and related data types, we feel the scientific community would be best served by the immediate launch of a central repository of short, highly structured 'Genome Notes' that must be standards-compliant. This could be done in the context of an existing journal, but we also suggest the more radical solution of launching a new journal. Such a journal could be designed to cater to a wide range of standards-related content types that are not currently centralized in the published literature. It could also support the demand for centralizing aspects of the 'gray literature' (documents developed by institutions or communities) such as the call by the GSCl for a central repository of Standard Operating Procedures describing the genomic annotation pipelines of the major sequencing centers. We argue that such an 'eJournal', published under the Open Access paradigm by the GSC, could be an attractive publishing forum for a broader range of standardization initiatives within, and beyond, ...
Date: April 1, 2008
Creator: Fenner, Marsha W; Garrity, George M.; Field, Dawn; Kyrpides, Nikos; Hirschman, Lynette; San-sone, Susanna-Assunta et al.
Partner: UNT Libraries Government Documents Department

Overcoming Scalability Challenges for Tool Daemon Launching

Description: Many tools that target parallel and distributed environments must co-locate a set of daemons with the distributed processes of the target application. However, efficient and portable deployment of these daemons on large scale systems is an unsolved problem. We overcome this gap with LaunchMON, a scalable, robust, portable, secure, and general purpose infrastructure for launching tool daemons. Its API allows tool builders to identify all processes of a target job, launch daemons on the relevant nodes and control daemon interaction. Our results show that Launch-MON scales to very large daemon counts and substantially enhances performance over existing ad hoc mechanisms.
Date: February 15, 2008
Creator: Ahn, D H; Arnold, D C; de Supinski, B R; Lee, G L; Miller, B P & Schulz, M
Partner: UNT Libraries Government Documents Department

FORTE spacecraft vibration mitigation. Final report

Description: This report documents work that was performed by CSA Engineering, Inc., for Los Alamos National Laboratory (LANL), to reduce vibrations of the FORTE spacecraft by retrofitting damped structural components into the spacecraft structure. The technical objective of the work was reduction of response at the location of payload components when the structure is subjected to the dynamic loading associated with launch and proto-qualification testing. FORTE is a small satellite that will be placed in orbit in 1996. The structure weighs approximately 425 lb, and is roughly 80 inches high and 40 inches in diameter. It was developed and built by LANL in conjunction with Sandia National Laboratories Albuquerque for the United States Department of Energy. The FORTE primary structure was fabricated primarily with graphite epoxy, using aluminum honeycomb core material for equipment decks and solar panel substrates. Equipment decks were bonded and bolted through aluminum mounting blocks to adjoining structure.
Date: February 1, 1996
Creator: Maly, J.R.
Partner: UNT Libraries Government Documents Department

Helical Pulse Line Structures for Ion Acceleration

Description: The basic concept of the ''Pulse Line Ion Accelerator'' is presented, where pulse power sources create a ramped traveling wave voltage pulse on a helical pulse line. Ions can surf on this traveling wave and achieve energy gains much larger than the peak applied voltage. Tapered and untapered lines are compared, and a transformer coupling technique for launching the wave is described.
Date: May 1, 2005
Creator: Briggs, R.J.; Reginato, L.L. & Waldron, W.L.
Partner: UNT Libraries Government Documents Department

Tall structure lightning induced by sprite-producing discharges.

Description: The large and rapid charge transfer of some +CGs can initiate upward positive leaders from tall structures while simultaneously initiating downward positive streamers below the base of the ionosphere in the form of sprites . Structures with >400 m height have a significantly enhanced probability of launching upward positive leaders, the presence of which is readily detected later if a dart leader propagates down the channel to ground, generating a -CG return stroke. Such tall structures can be repeatedly struck if, as often happens, sprite-producing +CGs repeatedly occur .
Date: January 1, 2003
Creator: Stanley, M. A. (Mark A.) & Heavner, M. J. (Matthew J.)
Partner: UNT Libraries Government Documents Department

On how to make the fastest gun in the west

Description: A new gasdynamic launcher is described, in which intact projectiles weighing at least one gram can be accelerated to mass velocities of 20 km/s. The system employs a conventional 2-stage light gas gun, with the barrel modified and filled with helium to act as a pump tube for a third stage. It is demonstrated that inter-stage kinetic energy efficiencies of 45% are possible and that these results can be achieved while maintaining the peak pressure applied to the projectile below 2.5 GPa. A simple analysis of this system is given, from which design parameters can be readily derived, and hydrocode calculations are presented to validate the model.
Date: January 1, 1997
Creator: Glenn, L.A.
Partner: UNT Libraries Government Documents Department

Debris growth sensitivity to launch and cascade rates

Description: Two-component models provide a good description of debris growth from the outset of launch to the present, predictions of future trends, and assessments of their sensitivity. Launch rate reductions produce less than proportional reductions in debris, for reasons that are discussed. The shift of debris to higher altitudes is assessed quantitatively, although the details of the growth are discussed elsewhere.
Date: October 24, 1996
Creator: Canavan, G. H.
Partner: UNT Libraries Government Documents Department

Non-US electrodynamic launchers research and development

Description: Electrodynamic launcher research and development work of scientists outside the United States is analyzed and assessed by six internationally recognized US experts in the field of electromagnetic and electrothermal launchers. The assessment covers five broad technology areas: (1) Experimental railguns; (2) Railgun theory and design; (3) Induction launchers; (4) Electrothermal guns; (5) Energy storage and power supplies. The overall conclusion is that non-US work on electrodynamic launchers is maturing rapidly after a relatively late start in many countries. No foreign program challenges the US efforts in scope, but it is evident that the United States may be surpassed in some technologies within the next few years. Until recently, published Russian work focused on hypervelocity for research purposes. Within the last two years, large facilities have been described where military-oriented development has been underway since the mid-1980s. Financial support for these large facilities appears to have collapsed, leaving no effective effort to develop practical launchers for military or civilian applications. Electrodynamic launcher research in Europe is making rapid progress by focusing on a single application, tactical launchers for the military. Four major laboratories, in Britain, France, Germany, and the Netherlands, are working on this problem. Though narrower in scope than the US effort, the European work enjoys a continuity of support that has accelerated its progress. The next decade will see the deployment of electrodynamic launcher technology, probably in the form of an electrothermal-chemical upgrade for an existing gun system. The time scale for deployment of electromagnetic launchers is entirely dependent on the level of research-and-development effort. If resources remain limited, the advantage will lie with cooperative efforts that have reasonably stable funding such as the present French-German program.
Date: November 1, 1994
Creator: Parker, J.V.; Batteh, J.H.; Greig, J.R.; Keefer, D.; McNab, I.R. & Zabar, Z.
Partner: UNT Libraries Government Documents Department

A Cost Effective Automatic Balloon Launcher

Description: Approximately 800,000 balloon-borne radiosondes are hand-launched each year, a cost and labor-intensive procedure. Development of a low-cost Automatic Radiosonde Launcher would allow the manual procedure to be replaced with a reliable and less expensive process. Balloon-borne radiosondes provide essential meteorological data used by forecasters and researchers around the globe. The National Weather service alone launches tens of thousands of sondes from sites across the US. Although worldwide launching of radiosondes has been done for many years, it remains a labor intensive and therefore expensive operation. Using its own funding and, more recently with the help of a Phase I SBIR grant, Visidyne, Inc. has begun investigating the feasibility of building an Automatic Radiosonde Launcher (ARL) that can be built at a cost that will be acceptable to the commercial marketplace. That work has led to the issuing of four patents covering important innovations that will allow us to meet that goal. Under the recent Phase I effort, solutions to many of the key problems have been tested in the laboratory and in real-world demonstrations in the field. The balloon filling, battery wetting, and launch release mechanisms were designed, built, and tested. A breadboard launcher was constructed and tested to prove feasibility of key system elements. Demonstration launches of radiosondes were performed using the breadboard launcher from the National Weather Service facility in Gray, ME, and from Hanscom AFB in Lexington, MA. The cost and size of a full scale shelter prevented us from building one during Phase I, however, we do have a design that will accomplish our goals. The Automatic Radiosonde Launcher will significantly reduce the cost of launching balloon-borne instruments. US and foreign weather services and atmospheric, climatological, and meteorological researchers will all benefit from this innovation.
Date: June 8, 2000
Creator: Michael, Berrigan J.
Partner: UNT Libraries Government Documents Department

Electromagnetic coilgun launcher for space applications

Description: A ground-based electrically-powered launcher could significantly reduce the complexity and cost of space launches for moderate-weight payloads. The EM launch complex could greatly reduce the amount of fuels handling, reduce the turnaround time between launches, allow more concurrence in launch preparation, reduce the manpower requirements for launch vehicle preparation and increase the reliability of launch by using more standardized vehicle preparations. The launch requires high acceleration, so the satellite package must be hardened. This paper presents results of a study to estimate the required launcher parameters, and estimate the cost of such a launch facility. This study is based on electromagnetic gun technology which is constrained to a coaxial geometry to take advantage of the efficiency of closely-coupled coils. The launcher energy and power requirements fall in the range of 40 {minus} 260 GJ and 20 {minus} 400 GW electric. Parametric evaluations have been conducted with a launcher length of 1-2 km, exit velocity of 1-6 kn/s, and payloads to low earth orbit of 100 1000 kg.
Date: October 1, 1995
Creator: Turman, B.N. & Lipinski, R.J.
Partner: UNT Libraries Government Documents Department

The SHARP scramjet launcher

Description: The worlds largest light gas gun at SHARP (Super High Altitude Research Project) is completed and in the past year has launched 9 scramjets. Typical masses and velocities are 5.9 kg at 2.8 km/sec.and 4.4 kg at 3.1 km/sec. In so doing SHARP launched the first fully functioning, hydrogen burning scramjet at mach 8. The SHARP launcher is unique in having a 4 inch diameter and 155 foot-long barrel. This enables lower acceleration launches than any other system. In addition the facility can deliver high energy projectiles to targets in the open air without having to contain the impact fragments. This allows one to track lethality test debris for several thousand feet.
Date: January 10, 1995
Creator: Cartland, H.; Fiske, P.; Greenwood, R.; Hargiss, D.; Heston, P.; Hinsey, N. et al.
Partner: UNT Libraries Government Documents Department

REDUCED ENERGY CONSUMPTION THROUGH PROJECTILE BASED EXCAVATION

Description: The Projectile Based Excavation (ProjEX) program has as its goal, the reduction of energy required for production mining and secondary breakage through the use of a projectile based excavation system. It depends on the development of a low cost family of projectiles that will penetrate and break up different types of ore/rock and a low cost electric launch system. The electric launch system will eliminate the need for high cost propellant investigated for similar concepts in the past. This document reports on the progress made in the program during the past quarter. It reports on projectile development and the development of the electric launch system design.
Date: October 12, 2002
Creator: Machina, Mark
Partner: UNT Libraries Government Documents Department

UAL USER GUIDE.

Description: The Unified Accelerator Libraries (UAL) provide a modularized environment for applying diverse accelerator simulation codes. Development of UAL is strongly prejudiced toward1 importing existing codes rather than developing new ones. This guide provides instructions for using this environment. This includes instructions for acquiring and building the codes, then for launching and interpreting some of the examples included with the distribution. In some cases the examples are general enough to be applied to different accelerators by mimicking input files and input parameters. The intention is to provide just enough computer language discussion (C++ and Perl) to support the use and understanding of the examples and to help the reader gain a general understanding of the overall architecture. Otherwise the manual is ''documentation by example.'' Except for an appendix concerning maps, discussion of physics is limited to comments accompanying the numerous code examples. Importation of codes into UAL is an ongoing enterprise and when a code is said to have been Imported it does not necessarily mean that all features are supported. Other than this, the original documentation remains applicable (and is not duplicated here.)
Date: January 9, 2003
Creator: Malitsky, N. & Talman, R.
Partner: UNT Libraries Government Documents Department

REDUCED ENERGY CONSUMPTION THROUGH PROJECTILE BASED EXCAVATION

Description: The Projectile Based Excavation (ProjEX) program has as its goal, the reduction of energy required for production mining and secondary breakage through the use of a projectile based excavation system. It depends on the development of a low cost family of projectiles that will penetrate and break up different types of ore/rock and a low cost electric launch system. The electric launch system will eliminate the need for high cost propellant considered for similar concepts in the past. This document reports on the progress made in the program during the past quarter. It reports on projectile development experiments and the development of the electric launch system design.
Date: January 9, 2002
Creator: Machina, Mark
Partner: UNT Libraries Government Documents Department

SHARP, a first step towards a full sized Jules Verne Launcher

Description: A vital element for space exploration and utilization is the ability to affordably place large quantities of consumables and building material into low earth orbit. Calculations and supportive data indicate this can be done with a large hydrogen gas gun referred to as the Jules Verne Launcher (JVL). We present a design for the JVL based upon the concept of side injecting preheated hydrogen along a long barrel. This dramatically reduces the peak pressures in the launcher as well as the pressures and g-loads at the vehicle. The JVL has the promise of reducing payload delivery costs to Low Earth Orbit (LEO) to below $500/kg. The Super High Altitude Research Project (SHARP) is a conventional two-stage hydrogen gas gun which is configured to launch 5 kg packages on suborbital trajectories. It is the first step towards the much larger Jules Verne system and will demonstrate several important features of the larger system. SHARP is currently in the middle of a series of tests aimed at its first milestone. This is to launch 5 kg at 4 km/sec horizontally. In its inclined configuration SHARP should launch vehicles to apogees in excess of 400 km and ranges in excess of 700 km.
Date: May 1, 1993
Creator: Bertolini, L. R.; Hunter, J. W.; Powell, J. R. & Tidman, D. A.
Partner: UNT Libraries Government Documents Department

Measurement of lateral launch loads on re-entry vehicles using SWAT

Description: The Sum of Weighted Accelerations Technique (SWAT) has been developed at Sandia National Laboratories to infer dynamic forces acting on free elastic structures from acceleration measurements. A derivative of SWAT known as SWAT TEEM (Sum of Weighted Accelerations using Tome Eliminated Elastic Modes) is utilized. This paper describes experiments demonstrating how this technology can be applied to measure lateral launch loads on Re-entry Vehicle (RV) payloads. A technique to determine the number of sensors and best locations is described. Experiments are performed to excite a structure to which a mockup RV is mounted. Acceleration measurements on the RV are used to reconstruct the lateral force acting at the RV base, and these results are compared to measured results.
Date: November 1, 1993
Creator: Mayes, R. L.
Partner: UNT Libraries Government Documents Department

Brief summary concerning strategic withholding (nuclear parsimony)

Description: This memorandum provides a brief summary on thoughts concerning `Strategic Withholding` (or perhaps, `Nuclear Parsimony`). It is chiefly meant to further support the view that there should be other significant doctrines besides `Brute-Force Retaliation`. The basic doctrinal argument is that it may be broadly disadvantageous to fire one`s missiles in equal, or `total` retaliation. It may be better to reply only softly, or not at all. The basic justification rests on an assumption of extended war, and on a logic addressed to what`s best for the surviving population and capability at any given point. In most strategic wargame exercises, it is rarely apparent that this principle is taken into account. The essential point of argument is that an extended war is not so different from peacetime posturing.
Date: June 2, 1971
Creator: Wouters, L. F.
Partner: UNT Libraries Government Documents Department

Covert air vehicle 2003 LDRD final report.

Description: This report describes the technical work carried out under a 2003 Laboratory Directed Research and Development project to develop a covert air vehicle. A mesoscale air vehicle that mimics a bird offers exceptional mobility and the possibility of remaining undetected during flight. Although some such vehicles exist, they are lacking in key areas: unassisted landing and launching, true mimicry of bird flight to remain covert, and a flapping flight time of any real duration. Current mainstream technology does not have the energy or power density necessary to achieve bird like flight for any meaningful length of time; however, Sandia has unique combustion powered linear actuators with the unprecedented high energy and power density needed for bird like flight. The small-scale, high-pressure valves and small-scale ignition to make this work have been developed at Sandia. We will study the feasibility of using this to achieve vehicle takeoff and wing flapping for sustained flight. This type of vehicle has broad applications for reconnaissance and communications networks, and could prove invaluable for military and intelligence operations throughout the world. Initial tests were conducted on scaled versions of the combustion-powered linear actuator. The tests results showed that heat transfer and friction effects dominate the combustion process at 'bird-like' sizes. The problems associated with micro-combustion must be solved before a true bird-like ornithopter can be developed.
Date: November 1, 2003
Creator: Spletzer, Barry Louis; Callow, Diane Schafer; Salton, Jonathan Robert & Fischer, Gary John
Partner: UNT Libraries Government Documents Department

Independent Safety Assessment of the TOPAZ-II space nuclear reactor power system (Revised)

Description: The Independent Safety Assessment described in this study report was performed to assess the safety of the design and launch plans anticipated by the U.S. Department of Defense (DOD) in 1993 for a Russian-built, U.S.-modified, TOPAZ-II space nuclear reactor power system. Its conclusions, and the bases for them, were intended to provide guidance for the U.S. Department of Energy (DOE) management in the event that the DOD requested authorization under section 91b. of the Atomic Energy Act of 1954, as amended, for possession and use (including ground testing and launch) of a nuclear-fueled, modified TOPAZ-II. The scientists and engineers who were engaged to perform this assessment are nationally-known nuclear safety experts in various disciplines. They met with participants in the TOPAZ-II program during the spring and summer of 1993 and produced a report based on their analysis of the proposed TOPAZ-II mission. Their conclusions were confined to the potential impact on public safety and did not include budgetary, reliability, or risk-benefit analyses.
Date: September 1, 1993
Partner: UNT Libraries Government Documents Department

Laser Safety Evaluation of the Oscmar M203PI Grenade Launcher Simulator (GLS) and the Associated Umpire Control Gun

Description: A laser safety evaluation and pertinent output measurements were performed (during March and April 2002) on the M203PI Grenade Launcher Simulator (GLS) and its associated Umpire Control Gun manufactured by Oscmar International Limited, Auckland, New Zealand. The results were the Oscmar Umpire Gun is laser hazard Class 1 and can be used without restrictions. The radiant energy output of the Oscmar M203PI GLS, under ''Small Source'' criteria at 10 centimeters, is laser hazard Class 3b and not usable, under SNL policy, in force-on-force exercises. However, due to a relatively large exit diameter and an intentionally large beam divergence, to simulate a large area blast, the output beam geometry met the criteria for ''Extended Source'' viewing [ANSI Std. 2136.1-2000 (S.l)]. Under this ''Extended Source'' criteria the output of the M203PI GLS unit was, in fact, laser hazard Class 1 (eye safe), for 3 of the 4 possible modes of laser operation. The 4'h mode, ''Auto Fire'', which simulates a continuous grenade firing every second and is not used at SNL, was laser hazard Class 3a (under the ''Extended Source'' viewing criteria). The M203PI GLS does present a laser hazard Class 3a to aided viewing with binoculars inside 3 meters from the unit. Farther than 3 meters it is ''eye safe''. The M203PI GLS can be considered a Class 1 laser hazard and can be used under SNL policy with the following restrictions: (1) The M203PI GLS unit shall only be programmed for: the ''Single Fire'' (which, includes ''Rapid Fire'') and the ''Auto Align'' (used in adjusting the alignment of the grenade launcher simulator system to the target) modes of operation. (2) The M203PI GLS shall never be directed against personnel, using binoculars, inside of 3 meters. DOE Order 5480.16A, Firearms Safety, (Chapter 1)(5)(a)(8)(d) and DOE-STD-1091-96, Firearms Safety (Chapter 4); already prevents ...
Date: June 1, 2002
Creator: Augustoni, Arnold L.
Partner: UNT Libraries Government Documents Department

Hypervelocity impact phenomena

Description: There is a need to determine the equations of state of materials in regimes of extreme high pressures, temperatures and strain rates that are not attainable on current two-stage light-gas guns. Understanding high-pressure material behavior is crucial to address the physical processes associated with a variety of hypervelocity impact events related to space sciences-orbital-debris impact, debris-shield designs, high-speed plasma propagation, and impact lethality applications. At very high impact velocities material properties will be dominated by phase-changes, such as melting or vaporization, which cannot be achieved at lower impact velocities. Development of well-controlled and repeatable hypervelocity launch capabilities is the first step necessary to improve our understanding of material behavior at extreme pressures and temperatures not currently available using conventional two-stage light-gas gun techniques. In this paper, techniques that have been used to extend both the launch capabilities of a two-stage light gas gun to 16 km/s, and their use to determine the material properties at pressures and temperature states higher than those ever obtained in the laboratory are summarized. The newly developed hypervelocity launcher (HVL) can launch intact (macroscopic dimensions) plates to 16 km/s. Time-resolved interferometric techniques have been used to determine shock-loading/release characteristics of materials impacted by such fliers as well as shock-induced vaporization phenomena in fully vaporized states. High-speed photography or radiography has been used to evaluate the debris propagation characteristics resulting from disc impact of thin bumper sheets at hypervelocities in excess of 10 km/s using the HVL. Examples of these experiments are provided in this paper.
Date: July 1995
Creator: Chhabildas, L. C.
Partner: UNT Libraries Government Documents Department

Report of trip to YTS - C91 test projectile

Description: As a part of the RAIL feasibility study, Operation Dorothe (March 1961) was conducted to determine if a liquid explosive could survive the acceleration of launch from a 155 mm howitzer. This operation was successful, although some structural difficulty was experienced with the test round (C-90). Upon completion of that exercise, it was decided to design a test round that could be used with the more viscous slurry-type explosives, and to fire several of these new rounds with inert filler prior to their use with slurry High Explosives (H.E.), precluding the difficulty previously experienced. The C-91 projectile, is a modified M107 H.E. round. It has been reduced in weight, equipped with an obturator, and provided with a large fill orifice. The rotating band has been altered to eliminate rotation. Internally, a plastic plug is used to control column height. A piston-type `O` ring seal prevents gun gas from reaching the interior to the projectile. Four of these projectiles were fired from a 155 mm howitzer at 15,500 g`s, plus. They survived not only the launch, but also impact and repeated ricochet in sand, gravel, and small rock. No leakage of the inert filler (glycerin) occurred. All rounds were destroyed with explosives upon completion of the exercise. Test data and engineering drawings are provided.
Date: May 1, 1961
Creator: Mickel, L.
Partner: UNT Libraries Government Documents Department