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United States automotive manufacturers, to maintain their pre-eminent position in world motor vehicle production, must expand their operations overseas. Tooling amortization expenses for the highly sophisticated domestic models are exorbitant because of low production volumes overseas. Therefore, it has been desirable to develop a vehicle which can be easily manufactured overseas for minimum capital expenditures. Chrysler International’s XLV truck cab has been styled, designed, and processed for low volume production overseas. This paper deals with the XLV program -- from the original idea to production in Turkey.

XM Satellite Radio launched its nationwide service in September of 2001. With 6.5 million subscribers at the end of the first quarter of 2006, XM is one of the fastest growing audio formats and entertainment services. This paper addresses XM's technology and content evolution, primarily for the radio unit and the signaling protocols, from the early years to the present time, and the applicability of this technology in fostering exciting new infotainment services. The radio architecture includes an antenna, an RF tuner module, a baseband chipset and a microprocessor. All of these subsystems underwent a complete transformation in the past four years from a size perspective, capability and cost. Specifically the following phases of the radio platform are addressed: a) Phase 1: The early years; b) Phase 2: The invention of the Plug and Play ; c) Phase 3: Connect and Play ; d) Phase 4; The wearable; e) Phase 5: Infotainment convergence of audio plus data services.

In October of 1997, the Federal Communications Commission (FCC) granted two national satellite radio licenses. The FCC allocated 25 MHz of the electromagnetic spectrum (2.3 GHz frequency band) for satellite digital broadcasting to two companies: 12.5 MHz to XM Satellite Radio and 12.5 MHz to Sirius Satellite Radio. This paper is an overview of the XM Satellite Radio technology. Four major components of the overall Network are described: a) The ground segment; b) The space segment; c) The terrestrial repeater segment and the d) The technology segment. Mobile antenna design challenges are also being addressed and optimum antenna configurations are presented.

The XMM-NEWTON satellite is the ESA X-ray spaceborne observatory covering the soft X-ray portion of the electromagnetic spectrum. XMM-NEWTON has been put in orbit on December, 10th 1999 by an Ariane 5 single launch. The spacecraft has a conventional thermal design that takes full advantage of the stable environment provided by its high altitude/long period orbit and by the limited variation of solar attitude angles in order to provide a stable platform for the telescope system. The precise geometry and alignment of the telescope system impose strict temperature requirements so that not only temperature gradients have to be kept small but also, and more importantly, time-variations of the gradients have to be minimised. In the paper, the thermal behaviour of the spacecraft as verified by its thermal test programme is compared with the early in-orbit temperature measurements.

In a continuing effort to expand the versatility of their aircraft, VTOL designers have for many years tried to combine the desirable features of various concepts into a single aircraft. This is a formidable task and most efforts have met with limited success. This paper explores the need for an aircraft combining the efficient VTOL capability of a helicopter with the efficient high speed characteristics of a fixed wing turboprop. The ability of the tilt rotor concept to fill this requirement and examples as to its potential usefulness in both military and civil missions, is discussed. The history of the concept and the status of the current Army/NASA/Bell XV-15 program and its role in proving the viability of the concept are reviewed.

XEROX has developed and implemented a network architecture for a real time control system which has expansion flexibility, high reliability, noise immunity, and low cost. This two level multiplex system with a single wire system bus at one level for distributed processors connected to local serial buses at the second level for remote functions and loads is described. The XEROX Microelectronics Center has developed a set of custom VLSI chips to implement the multiplexing architecture. Control software was developed using both assemblers and high level language tools. The software and chip set have been designed, built and integrated into XEROX'S latest generation of products.

The significance of thermal management performance in electric vehicles (EVs) has grown considerably, leading to increased complexity in thermal systems and a rapid rise in safety and quality-related concerns. The present real-vehicle-based development methods encounter several constraints in their approach when dealing with highly complex systems. Huge number of verification and validation work To overcome these limitations and enhance the thermal system development process, a novel virtual development environment established using the XiLS (X in the Loop Simulation) methodology. This XiLS methodology basically based on real-time coupling between physical thermal system hardware and analytical models for the other systems of vehicle. To control vehicle model and thermal system, various options were realized through hardware, software and model for VCU (Vehicle control unit) and TMS (Thermal management system) control unit.

MBB and Rockwell, under DARPA/NAVAIR and GMOD contract, are currently designing an experimental aircraft which will be dedicated to demonstrate “enhanced fighter maneuverability” (EFM) and supermaneuverability in particular. The aircraft is designed to break one of the last barriers left in aviation, the stall barrier. It will be able to perform tactical maneuvers up to 70° angle of attack and thus achieve very small radii of turn. Such highly instantaneous 3-dimensional maneuvers are of significant tactical value in future air combat with all aspect weapons. Key to the penetration into this unexplored flight regime is thrust vectoring in pitch and yaw. This feature is also used to enhance agility in critical flight conditions and to enhance the decoupling of fuselage aiming and flight path control as required for head-on gun firing.

The Army's new Advanced Attack Helicopter - the YAH-64 - achieves high performance with low cost and excellent maintainability. These desirable characteristics result from the Design Simplicity which has been inherent in the design approach since conception in 1972 and throughout the Phase 1 and Phase 2 development and flight test program. This inherent simplicity is the direct result of several fundamental decisions regarding basic configuration, plus intensive discipline at all levels of the design.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.