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THE OBJECTIVE OF THIS EFFORT IS TO ESTABLISH PAYOFF MEASURMENT PARAMETERS AND ATTENDANT WEIGHTING VALUES/ RANGES FOR DISTRIBUTE DATA PROCESSING SYSTEMS FOR VARIOUS BALLISTIC MISSILE DEFENSE (BMD) SYSTEM ARCHITECTURES. THESE PARAMETERS AND WEIGHTING SCHEMES WILL BE ESTABLISHED TO ACHIEVE OPERATIONAL EFFECTIVENESS, AS WELL AS THE DEFINITION, DESIGN, AND CONSTRUCTION PROCESSES AND METHODOLOGIES DEVEL ...

THE PRIMARY OBJECTIVE OF THIS PROJECT IS TO PROVIDE THE DESIGNER OF AN TI-RADIATION HOMING MISSILES WITH THE INFORMATION NECESSARY TO STRUCTURE FUTURE STUDIES AND TECHNOLOGY PROGRAMS AIMED AT DEVELOPING AN ANTI- RADIATION MISSILE CAPABLE OF HOMING ON THREAT RADIATION MISSILE CAPABLE OF HOMING THREAT RADARS UTILIZING SPREAD SPECTRUM TECHNIQUES. THIS INVOLVES THE FOLLOWING TWO TASKS: 1. DEFINE THE C ...

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EER PROPOSES TO CONDUCT A 4 1 MAN MONTH EXPLORATORY DEVELOPMENT EFFORT WHICH WILL FOCUS UPON THE FESIBILITY OF ADAPTING A PREVISOUSLY DEVELOPED MANAGEMENT TOOL WHICH IS CAPABLE OF IDENTIFYING BOTH HIERARCHIAL AND RELATIONAL DATA BASE ATTRIBIUTES. SPECIFICALLY,EER PROPOSES TO ADAPT A REQUIREMENTS DATA BASE TOOL THAT IS CAPABLE OF BEING IDENIFIED IN TERMS OF A MAJOR SYSTEM CONSTRUCTOR IN TERMS OF WR ...

FABRICS CONSISTING OF ACTIVATED CARBON FIBERS ARE BEING DEVELOPED FOR USE IN CHEMICAL PROTECTIVE GARMENTS AS POTENTIAL REPLACEMENT FOR THE CURRENT COATED FOAM. THESE FABRICS NOT ONLY MUST ABSORB TOXIC CHEMICAL VAPORS ADEQUATELY BUT ALSO PROVIDE GOOD AIR MOISTURE PERMEABILITY TO MINIMIZE THE PHYSIOLOGICAL STRESS ON THE NEARER. HOWEVER, LITTLE IS KNOWN ABOUT THE MECHANISM OF THE COMBINED PROCESSES O ...

MANY AREAS OF ORTHOPAEDIC SURGERY WOULD BENEFIT FROM AN INJECTABLE,BIOCOMPATIBLE BONE CEMENT OR BONE REPLACEMENT MATERIAL WHICH COULD PROVIDE IMMEDIATE STRUCTURAL REINORCEMENT TO SKELETAL REGIONS AND THEN GRADUALLY BE INCORPORATED INTO HOST BONES. THE HARVARD MEDICAL SCHOOL BIOMECHAINCS LABORATORY HAS DEVELOPED A PARTICIPATE BONE\ GELATIN COMPOSITE WHICH CURRENTLY UNDERGOING TESTS IN ANIMALS. THIS ...

THIS PROJECT WILL DEVELOP A TEST PROCEDURE TO DETERMINE STRENGHT OF ROCKET MOTOR CASE MATERIALS AT TEMPERATURES APPROACHING THE MELTING POINT OF THE MATERIALS TO EXTEND THEDATA PRESENTED IN MIL-HDBK-5C. LASER TECHNIQUES TO MEASURE STRAIN BY OBSERVING FLAGS ON THE TEST SPECIMENS AT ELEVATED TEMPERATURES WILL BE USED. SPECIAL ATTENTION WILL BE PAID TOMETHODS OF AFFIXING OR CREATING OBSERVATION FLAGS ...