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Relating to yet beyond the requirements of putting controls and displays at selected and selectable locations in the station, and to associated subsystem interfaces, is the ergonomic integration of these elements with the operator, and ALL with the diverse, proximal station architecture. Basic to optimal, long-term solutions to this integration is the requirement of the felicitous accommodation of a range of crew sizes from a 5% tile Asian female to a 95% tile Caucasian male. No less important is for the workstation's layout and architecture being optimized for the “new-shape-of-man” - the “neutral body position” - in weightlessness and with the associated geometry and dynamics of this significantly altered state, its capabilities and its new facility. This paper previews the on-going status, development and details of a body-ported workstation prototype and its semi stand-alone elements.

Currently, many factors influence the NASA Kennedy Space Center (KSC) workforce. These factors include the drive for return to flight, a Shuttle Program end date of 2010, and the Vision for Space Exploration which calls for the development of a new launch vehicle. Additionally, external factors exist as well, such as the area's cost of living, the availability of skilled resources, and the unemployment rate affect the overall workforce climate. To manage the human capital in a manner consistent with safety and mission success, and to strategically position NASA KSC to execute its future mission, it is necessary to understand how all of these different influencing factors work together to produce an overall workforce climate. We have been using System Dynamics models in order to capture some of these factors. These system dynamics models are also the starting point of agent-based models.

Selection of working fluid is one of the main criterions for designing of heat pipes thermal control systems (TCS) for space application. In this paper we will describe how we solved the task of development of the TCS with working fluid of high thermal physical properties. In 2004-2006 we developed the Engineering model of Deployable Radiator based on Loop Heat Pipe by CAST purchase order. It was developed for qualification tests. Ammonia application as LHP working fluid is stipulated by its high thermal physical properties. However Ammonia freezing temperature is of minus 77ºC. Such fact impedes Ammonia application when operation temperatures of LHP Radiator are lower than this value, for example, It takes several tens of hours to orbit a spacecraft and prepare it for work (at that moment the spacecraft is out of power supply) and the working fluid can be frozen in a condenser-radiator when the spacecraft being in the shadow over a long period of time.

Several studies have been performed to investigate the effects of using hydrogen in spark ignition (SI) engines. One general conclusion that emerged was that stoichiometric operation of premixed charge hydrogen engines features increased losses compared to other fuels such as methane. Most studies attribute this higher loss to increased rates of heat transfer from the working fluid to the combustion chamber walls. Indeed, heat flux measurements during combustion and expansion recorded much higher values for hydrogen compared to methane stoichiometric operation. With regard to fluid properties, using the same net heat release equation as for gasoline engines results in an over prediction of heat losses to the combustion chamber walls. Also, the variation of specific heats ratio greatly influences calculated values for the rate of heat release. Therefore, a more detailed analysis of heat losses is required when comparing hydrogen to other fuels.

The substantiation of heat pipe usage in passive radiative cooling systems on temperature level (190…240) K for space optical sensors is presented. Heat pipes can be sound practice like heat conducting lines between sensor and radiator particularly at distances more 0.2 m and irreplaceable at distances (0.5…2) m. Embedding heat pipe with radiator allows to create the uniform temperature basis in case of several sensors connection to single radiator and to improve radiator efficiency. It is analyzed approach to design of thermocontrol and cooling radiative systems with heat pipes to reduce sensitiveness to external light disturbances and to enlarge area of radiative system application. The results of design, thermovacuum test and flight operation of thermocontrol radiative system samples are under discussion as well.

Current and future generations of transport aircraft are characterized by a high level of automation. This automation is intended to assist the flight crew and make it possible for a crew of two persons to operate these aircraft for all types of flights, including those of extremely long duration. While one of the design goals of automation is to reduce crew workload, little is known about the true relationship between workload and automation. This paper discusses the approaches taken by Airbus Industrie when designing increasing levels of automation into their aircraft. It also addresses the Airbus program of workload research and the need to direct specific attention to the relationship between workload and automation.

Cockpits have changed dramatically over the last ten years. The electro-mechanical instruments have largely been replaced with electro-optical controls and displays. This change in the pilot-vehicle interface, coupled with a second development, the emergence of a very powerful airborne computer system, an Electronic Crewmember, has had a significant impact on workload in the cockpit. Workload has shifted from physical to mental, and many workload measurement tools applied previously may no longer be appropriate. This paper discusses the prediction, real time measurement and dynamic allocation of cockpit workload in an aircraft with a crew of two -- one human and one electronic.

Standardization and “Zero-Defects” are buzz-words among today's truck manufacturers. Electrical components is an area where these words must become reality. Components costing less than 1% of the final truck price should not cause problems for the end user or the manufacturer. The way to insure this is communication and design. Design out problems with new components.

A new line of on-highway transmissions has been designed and developed by Allison Transmission Division. This new product line, identified as the World Transmission Series (WT), has been designed with emphasis on cost-effectiveness, greater integration with vehicle systems and advanced technology to meet market demands into the 21st century. New design concepts both in power train component arrangement and electronic controls have been coupled utilizing concurrent engineering and systems engineering principles. The result is a customer-driven product line which, when produced by Allison, will exceed world class standards of quality, performance and value.

The idea of a world truck is a fascinating challenge - whereas cars are purchased more or less as seen; truck purchasers demand more individual configurations. In national and global terms, that means a highly complex truck market. Historically, a few European and North American manufacturers produced almost all the trucks for the world market. That changed through the 60's and 70's, with more local assembly plants around the world and increasing worldwide manufacturing capabilities. Concurrently, international component design standards have made some progress towards compatibility. Much greater co-operation is needed, however, before a genuinely international set of standards can be applied. As the task assigned to trucks is the same worldwide, namely to transport goods from A to B; it should be desirable and possible to work towards a greater commonality of vehicle - to ultimately achieve a world truck. The only unknown is the time scale.

In 1981, Ford Motor Company introduced a new family of fuel efficient four cylinder engines world wide. These engines, based on a compound valve arrangement in a hemispherical combustion chamber, were specifically designed for installation in light weight front-wheel-drive vehicles. Ford Research efforts were integrated with the resources of Ford U.S. and Ford of Europe to design and develop the engine in a compressed time frame. The technical and organizational efforts to accomplish this task, as well as, the design and development are discussed.

The first flight of a delta wing aircraft took place in the United States at the Muroc AFB Flight Test Center on 18 September 1948. The aircraft, Convair No. 7002, Air Force S/N 46-682 and designated the XF-92A was piloted by Convair's Manager of Flight Research, E.D. “Sam” Shannon. The author witnessed this historic flight as a Flight Test Engineer on the project. Studies and wind tunnel tests for a supersonic interceptor were conducted at the Vultee Division of Consolidated Vultee Aircraft Corporation (Convair) in 1945. These studies led to the selection of the 60° delta wing plan form. This paper reviews the major differences between the thin wing XF-92A and the thick wing DM-1 glider (never flown) designed by Alexander M. Lippisch in Germany at the close of World War II. The XF-92A used a fully hydraulic irreversible control system for its elevons and rudder. The only airplanes up to this time with fully hydraulic controls were the Northrop XB-35 and the YB-49 flying wings.

The Convair/Navy XFY-1 VTOL fighter was ahead of its time. In the early 1950s it became the first airplane to take off vertically, hover, transition to high speed level flight, transition back to hover, and land vertically. Pilot “Skeets” Coleman made a number of successful flights at Moffett Field South of San Francisco, at Brown Field near the California/Mexican border, and at San Diego's Lindbergh Field. This “first of a kind” aircraft soon adopted the name “POGO”. The POGO with its stall proof delta wing had near perfect aerodynamic characteristics in hover, transition and level flight. There were no “black boxes” needed for stability augmentation. The POGO was one of the very first aircraft to use hydraulic power flight controls - a system used today on all modern fighter and transport aircraft.

Most of the major industrialized areas of the world have been experiencing serious motor vehicle pollution problems over the last decade. The motor vehicle pollution control programs which have have been developed to deal with the effects have led to tremendous advances in gasoline car control technologies. Similar technologies are under intensive development for diesel cars and trucks. Several developing countries are now experiencing similar air pollution problems. This paper surveys the most recent data regarding adverse environmental impacts resulting from motor vehicles, reviews technologies developed to address these problems, and summarizes the current status around the world.

Battery electric vehicles (BEVs) are equipped with Mobile Air Conditioning systems (MACs) to ensure a comfortable cabin temperature in all climates and ambient conditions as well as the optional conditioning of the traction battery. An assessment of the global electrical energy consumption of various MACs has been derived, where the basis of the assessment procedure is the climate data GREEN-MAC-LCCP 2007 (Global Refrigerants Energy & Environmental - Mobile Air Condition - Life Cycle Climate Performance) and the improved LCCP2013 (Life Cycle Climate Performance. The percentage driving time during 6 AM and 24 PM is divided into six different temperature bins with the solar radiation and relative humidity for 211 cities distributed over Europe, North, Central, and South America, Asia, South West Pacific, and Africa. The energy consumption of the MACs is determined by a thermal vehicle simulation. In this work, four different MACs are simulated and compared.

The world consumption rate of oil is increasing so fast that the supply will not keep pace. During 1977, the world energy consumption exceeded 265 quadrillion BTU s--the equivalent of over 130 million barrels of oil per day. By the year 2000, world energy consumption is expected to more than double. Some time between 1980 and the turn of the century, world oil production will stop growing and slowly begin to shrink. The inescapable conclusion is that petroleum will not be able to maintain its share of the rapidly growing demand for energy. Recognizing that there is a close relationship between energy consumption and the performance of national economies, especially in industrialized nations, other fuels will be needed to meet growth demands. The world must shift from a predominantly petroleum-based economy to one which will phase in other energy sources, with increased emphasis on coal and nuclear power. This transition will require some complex decisions.

United States construction equipment manufacturers are subject to a maze of product-oriented regulations in marketing their U.S.-built products in foreign countries. These same obstacles face their foreign-built products. In the past, these foreign regulations were more apt to be trade barriers to protect domestic markets than bonafide regulations to protect the users. These trade barriers are gradually being lifted because manufacturers in virtually all countries have now expanded beyond their domestic markets. Thus, the same manufacturers that formerly encouraged trade barriers must now cope with them. This expansion of markets now encourages the elimination of trade barriers and the harmonization of regulations. For the future, regulations will be retained and expanded. They will, however, be harmonized with international voluntary standards rather than having different regulations for each country.

The quality and availability of distillate fuels in the coming decades has become an increasing concern to the U.S. Navy. In response, the Energy Research and Development Office of the David Taylor Naval Ship Research and Development Center (DTNSRDC) has conducted a worldwide survey of commercial marine fuels. An effort was made to obtain 50 commercial marine fuel samples from various suppliers worldwide. The purpose of the survey was to assess the current quality of available fuels by analytically characterizing each of the fuel samples obtained. This assessment consisted of the measurement of more than 44 fuel properties. This paper contains a summary of the analytical results which were obtained. In addition, the current analytical results are compared with refinery specifications, with the current Navy specification, and with the results of a similar survey conducted in 1983. Finally, the resulting conclusions and recommendations are presented.

It is the goal of this paper, to discuss the impact of electronics on modern day commercial vehicles an buses. Seen from the position of advanced engineering of an European commercial vehicle manufacturer, the emphasis will be placed on the mechanical-electronical system itself, rather than the electronics themselves. User friendly, logic protected systems will minimize operator unfamiliarity and misapplication and will offer not only component control, but shortly the integration of all of these subsystems in the total vehicle control. Total vehicle control will be the ultimate result, when the driver, the truck and the environment are brought together. Such vehicles will be more responsive, safer and easier to drive than today's commercial vehicles and buses and offer a cost effective utilization of these new technologies to the customer.