Deployable large area solar array structure Preliminary developmental report, phase I

Roller drum, actuation system, support structure, electrical provisions, and substrate design concepts for deployable large area solar array structur

Human Powered Vehicle Frame Design

This report discusses the Human Powered Vehicle Frame Design senior project’s contributions to the design, manufacture, testing, and competition of the Cal Poly Human Powered Vehicle Club’s 2015 vehicle, Sweet Phoenix. The project’s guiding rules and timeline were dictated by the ASME Human Powered Vehicle Challenge (HPVC), held in April 2015. The Club sought to improve upon its previous vehicle, Aria, which suffered from a range of faults including a catastrophic structural failure at the 2014 HPVC. Largely in response to this failure, the Frame Design project’s major focus was Sweet Phoenix’s frame, from concept to manufacturing. During the design process in the Spring and Fall of 2014, several other issues were tackled in order to define the frame’s design parameters. These secondary efforts included the fairing shape, vehicle stability requirements, handling characteristics, and rider ergonomics. A handling prototype was constructed in late Fall 2014, which successfully validated the solutions to these secondary requirements before the final design was constructed. Ultimately, Sweet Phoenix’s frame is a hybrid design – a composite monocoque fairing to which several weldments are mechanically fastened. The team used extensive finite element analysis to evaluate structural properties for both of these frame subsystems during the final development stages. Sweet Phoenix was produced during the Winter quarter of 2015, with much physical help from the HPV Club members and financial support from several sponsors. The production effort was quite successful, in part thanks to two significant manufacturing improvements – sponsored out-of-house machining of the fairing tools, and a frame-to-fairing alignment jig. The vehicle’s construction quality was recognized at HPVC with a “Best Craftsmanship” award. Testing of the final vehicle revealed very low stiffness of the weldments’ fairing mounts, which was resolved by adding additional bracing locations to the fairing. In addition, the team discovered several drivetrain-related issues that were attacked with numerous attempted solutions, but were not solved prior to HPVC. The drivetrain also contributed to localized delamination of the fairing near a chain idler pulley mount. Unfortunately, these drivetrain issues resulted in several broken chains and poor performance in the acceleration-heavy Endurance Event at HPVC. On the other hand, Sweet Phoenix placed 1st in Design and Men’s Sprint, both satisfying results for the Club, and the Frame Design project was an overall success

The 31st Aerospace Mechanisms Symposium

The proceedings of the 31st Aerospace Mechanisms Symposium are reported. Topics covered include: robotics, deployment mechanisms, bearings, actuators, scanners, boom and antenna release, and test equipment. A major focus is the reporting of problems and solutions associated with the development and flight certification of new mechanisms

Wind Turbine Structural Dynamics

A workshop on wind turbine structural dynamics was held to review and document current United States work on the dynamic behavior of large wind turbines, primarily of the horizontal-axis type, and to identify and discuss other wind turbine configurations that may have lower cost and weight. Information was exchanged on the following topics: (1) Methods for calculating dynamic loads; (2) Aeroelasticity stability (3) Wind loads, both steady and transient; (4) Critical design conditions; (5) Drive train dynamics; and (6) Behavior of operating wind turbines

Proceedings of the Seventh Annual Summer Conference. NASA/USRA: University Advanced Design Program

The Advanced Design Program (ADP) is a unique program that brings together students and faculty from U.S. engineering schools with engineers from the NASA centers through integration of current and future NASA space and aeronautics projects into university engineering design curriculum. The Advanced Space Design Program study topics cover a broad range of projects that could be undertaken during a 20-30 year period beginning with the deployment of the Space Station Freedom. The Advanced Aeronautics Design Program study topics typically focus on nearer-term projects of interest to NASA, covering from small, slow-speed vehicles through large, supersonic passenger transports and on through hypersonic research vehicles. Student work accomplished during the 1990-91 academic year and reported at the 7th Annual Summer Conference is presented

Bibliography of Lewis Research Center technical publications announced in 1985

This compilation of abstracts describes and indexes the technical reporting that resulted from the scientific and engineering work performed and managed by the Lewis Research Center in 1985. All the publications were announced in the 1985 issues of STAR (Scientific and Technical Aerospace Reports) and/or IAA (International Aerospace Abstracts). Included are research reports, journal articles, conference presentations, patents and patent applications, and theses

An advanced study of an Application Technology Satellite /ATS-4/ mission, volume I, book 2 Final study report, May - Nov. 1966

Application Technology Satellite /ATS/ SPACECRAFT tradeoff and analysis - configuration paraboloid antenna, guidance and control power, spacecraft design, and apogee motor selectio

Motorless flight research, 1972

The proceedings of a symposium on motorless flight research are presented. The subjects discussed are: (1) glider aerodynamic and design, (2) instrumentation, (3) structural concepts and materials, (4) soaring meteorology, (5) self-launching and ultralight sailplanes, and (6) performance testing

Ninteenth Aerospace Mechanisms Symposium

The proceedings of the 19th Aerospace Mechanisms Symposium are reported. Technological areas covered include space lubrication, bearings, aerodynamic devices, spacecraft/Shuttle latches, deployment, positioning, and pointing. Devices for spacecraft docking and manipulator and teleoperator mechanisms are also described