Reusable Centaur study. Volume 1: Executive summary

A study of the Reusable Centaur for use as an initial upper stage with the space shuttle was conducted. The currently operative Centaur stage, with modifications for space shuttle orbiter compatibility and for improved performance, represents a cost effective development solution. The performance needs and available development funds are discussed. The main features of three Reusable Centaur configurations with increasing capability at increasing development costs are summarized

Integrated controls and health monitoring for chemical transfer propulsion

NASA is reviewing various propulsion technologies for exploring space. The requirements are examined for one enabling propulsion technology: Integrated Controls and Health Monitoring (ICHM) for Chemical Transfer Propulsion (CTP). Functional requirements for a CTP-ICHM system are proposed from tentative mission scenarios, vehicle configurations, CTP specifications, and technical feasibility. These CTP-ICHM requirements go beyond traditional reliable operation and emergency shutoff control to include: (1) enhanced mission flexibility; (2) continuously variable throttling; (3) tank-head start control; (4) automated prestart and post-shutoff engine check; (5) monitoring of space exposure degradation; and (6) product evolution flexibility. Technology development plans are also discussed

Modelling and use of SysML behaviour models for achieving dynamic use cases of technical products in different VR-systems

Digital methods and models help the product designers in performing early evaluations on a product that eventually help to gain understanding about a product’s behaviour and its interactions with neighbouring systems in its later life-phases. Virtual Reality (VR) is a technology that can facilitate the early evaluation process by showing later life situations of a product as early as at the design stage. However, the application of VR in the industry is currently limited due to high model preparation effort and poor reusability of already prepared models. Therefore, this thesis pursues towards the development of a method that can facilitate the early evaluations of the product in VR and thus, facilitate the use of VR in the product development process. This method aims at achieving generic behavioural descriptions for use in VR that can be reused as well to form dynamic use cases of a product in different VR-systems. The focus lies on reducing the overall preparation effort of VR-models and on achieving high reusability of already created models. The core components of the thesis consist of the use of Model Based Systems Engineering (MBSE) to develop generic behavioural model descriptions, their use in building different use cases of a product in one VR-system and their reuse in different VR-systems as well. The Systems Modeling Language (SysML) is used to describe the behavioural models, the modelling process is described systematically and is also summarized in the form of general-purpose guidelines for later use. Furthermore, a dedicated physics engine is used to perform the physical calculations on virtual objects in VR and is integrated with the SysML. These SysML behaviour models together with the physics engine are used to achieve a real-time product use case simulation inside VR. The same SysML behaviour models are used across different VR-systems to achieve real-time simulations and to validate their reuse. Two VR prototypes are developed to demonstrate the effectivity and use of the presented method. Finally, one of the prototypes is put to the empirical evaluation performed with the help of experts from academia as well as the industry.Digitale Methode und Modellen ermöglichen den Produktdesignern eine frühzeitige Evaluierung des Produkts, damit sie das Verhalten des Produkts und seine Interaktionen mit benachbarten Systemen in seinen späteren Lebensphasen besser verstehen können. Virtual Reality (VR) ist eine Technologie, die zum frühen Evaluierungsprozess beitragen kann, indem spätere Lebenssituationen eines Produkts schon in der Entwurfsphase angezeigt werden können. Die Anwendung von VR in der Industrie ist jedoch derzeit aufgrund des hohen Modellaufbereitungsaufwands und der limitierten Wiederverwendbarkeit vorhandener Modelle begrenzt. Daher befasst sich diese Arbeit mit der Entwicklung einer Methode, die die frühzeitige Evaluierung des Produkts innerhalb von VR und die Verwendung von VR im Produktentwicklungsprozess erleichtern kann. Diese Methode befasst sich mit dem Prozess der Entwicklung allgemeiner Verhaltensbeschreibungen zur Verwendung in VR, die auch wiederverwendet werden können, um dynamische Anwendungsfälle eines Produkts in den verschiedenen VR-Systemen abzubilden. Der Fokus liegt auf der Reduzierung des gesamten Aufbereitungsaufwands von VR-Modellen und auf das Verwirklichen einer hohen Wiederverwendbarkeit bereits vorhandener Modelle. Die Kernkomponenten der Arbeit bestehen in der Verwendung von Model Based Systems Engineering (MBSE) zur Entwicklung allgemeingültiger Verhaltensmodellbeschreibungen, ihrer Verwendung beim Erstellen verschiedener Anwendungsfälle eines Produkts in einem VR-System und ihrer Wiederverwendung in den verschiedenen VR-Systemen. Die Systems Modeling Language (SysML) wird zur Beschreibung der Verhaltensmodelle verwendet, der Modellierungsprozess wird systematisch beschrieben und auch in Form allgemeiner Anwendungsrichtlinien für die spätere Verwendung zusammengefasst. Darüber hinaus wird eine dedizierte Physik-Engine verwendet, um die physikalischen Berechnungen für virtuelle Objekte in VR durchzuführen, welche auch mit SysML integriert ist. Diese SysML-Verhaltensmodelle zusammen mit der Physik-Engine bilden eine echtzeitfähige Produktanwendungssimulation in VR. Dieselben SysML-Verhaltensmodelle werden für verschiedene VR-Systeme verwendet, um Echtzeitsimulationen abzubilden und ihre Wiederverwendung zu validieren. Zwei VR-Prototypen wurden entwickelt, um die Wirksamkeit und Verwendung der vorgestellten Methoden zu demonstrieren. Schließlich wurde einer der Prototypen einer empirischen Untersuchung unterzogen, die mithilfe von Experten aus Wissenschaft und Industrie durchgeführt wurde

Absorption capacity, kinetics and mechanical behaviour in dry and wet states of hydrophobic DEDMS/TEOS-based silica aerogels

This work is a new approach to the study of the structural, mechanical and absorption properties of hybrid organic/inorganic silica-based aerogels. Diethoxydimethylsilane and tetraethoxysilane have been used as precursors. Changes in properties such as specific surface area, porous volume, pore radius, and surface texture and chemistry were researched as a function of the relative organic content. In addition, the absorption properties were tested for different organic liquids. The discrepancy in the absorption mechanisms and the kinetics of pure inorganic and hybrid samples were discussed. It was confirmed that swelling occurs in samples with high organic content, which, in turn, governs the absorption process. Finally, the mechanical behaviour was studied by uniaxial compression. A significant rise of the rupture strain up to 0.45 and a 10-fold decrease in the Young’s modulus to 7.8 MPa were measured in the dry samples by increasing the organic content. The mechanical response of the samples after saturation by the absorption of two reference oily liquids, namely, common motor oil and liquid polydimethylsiloxane, was also compared with the behaviour of dry samples. The presence of liquid within the sample reduced the value of the mechanical parameters in almost all cases. Moreover, the inclusion of organic chains also made the wet aerogels highly deformable. In summary, these first results suggest that tuning the organic ratio of the hybrid aerogels allows the control of not only the structural and mechanical properties but also the absorption properties.Junta de Andalucía P09-TEP-546

Reusable Agena study. Volume 2: Technical

The application of the existing Agena vehicle as a reusable upper stage for the space shuttle is discussed. The primary objective of the study is to define those changes to the Agena required for it to function in the reusable mode in the 100 percent capture of the NASA-DOD mission model. This 100 percent capture is achieved without use of kick motors or stages by simply increasing the Agena propellant load by using optional strap-on-tanks. The required shuttle support equipment, launch and flight operations techniques, development program, and cost package are also defined

NASA Technology Area 07: Human Exploration Destination Systems Roadmap

This paper gives an overview of the National Aeronautics and Space Administration (NASA) Office of Chief Technologist (OCT) led Space Technology Roadmap definition efforts. This paper will given an executive summary of the technology area 07 (TA07) Human Exploration Destination Systems (HEDS). These are draft roadmaps being reviewed and updated by the National Research Council. Deep-space human exploration missions will require many game changing technologies to enable safe missions, become more independent, and enable intelligent autonomous operations and take advantage of the local resources to become self-sufficient thereby meeting the goal of sustained human presence in space. Taking advantage of in-situ resources enhances and enables revolutionary robotic and human missions beyond the traditional mission architectures and launch vehicle capabilities. Mobility systems will include in-space flying, surface roving, and Extra-vehicular Activity/Extravehicular Robotics (EVA/EVR) mobility. These push missions will take advantage of sustainability and supportability technologies that will allow mission independence to conduct human mission operations either on or near the Earth, in deep space, in the vicinity of Mars, or on the Martian surface while opening up commercialization opportunities in low Earth orbit (LEO) for research, industrial development, academia, and entertainment space industries. The Human Exploration Destination Systems (HEDS) Technology Area (TA) 7 Team has been chartered by the Office of the Chief Technologist (OCT) to strategically roadmap technology investments that will enable sustained human exploration and support NASA s missions and goals for at least the next 25 years. HEDS technologies will enable a sustained human presence for exploring destinations such as remote sites on Earth and beyond including, but not limited to, LaGrange points, low Earth orbit (LEO), high Earth orbit (HEO), geosynchronous orbit (GEO), the Moon, near-Earth objects (NEOs), which > 95% are asteroidal bodies, Phobos, Deimos, Mars, and beyond. The HEDS technology roadmap will strategically guide NASA and other U.S. Government agency technology investments that will result in capabilities enabling human exploration missions to diverse destinations generating high returns on investments

Reusable Ionogel-based Photo-actuators in a Lab-on-a-disc

This paper describes the design, fabrication and performance of a reusable ionogel-based photo-actuator, in-situ photopolymerised into a lab-on-a-disc microfluidic device, for flow control. The ionogel provides an effective barrier to liquids during storage of reagents and spinning of the disc. A simple LED (white light) triggers actuation of the ionogel for selective and precise channel opening at a desired location and time. The mechanism of actuation is reversible, and regeneration of the actuator is possible with an acid chloride solution. In order to achieve regeneration, the Lab-on-a-Disc device was designed with a microchannel connected perpendicularly to the bottom of the ionogel actuator (regeneration channel). This configuration allows the acid solution to reach the actuator, independently from the main channel, which initiates ionogel swelling and main channel closure, and thereby enables reusability of the whole device.Economía y Competitividad), Spain. This project has receivedfunding from the European Union Seventh Framework Programme(FP7) for Research, Technological Development and Demonstrationunder grant agreement no. 604241. JS and FBL acknowledge fund-ing support from Gobierno de Espa˜na, Ministerio de Economía yCompetitividad, with Grant No. BIO2016-80417-P and personallyacknowledge to Marian M. De Pancorbo for letting them to use herlaboratory facilities at UPV/EHU. A.T., L.F., and D.D. are grateful forfinancial support from the Marie Curie Innovative Training Net-work OrgBIO (Marie Curie ITN, GA607896) and Science FoundationIreland (SFI) under the Insight Centre for Data Analytics initiative,Grant Number SFI/12/RC/2289

Direct Laser Fabrication of a Gas Turbine Engine Component - Microstructure and Properties - Part I

This paper presents the development of a new technique for the production of abrasive turbine blade tips by direct laser processing. This superalloy cermet component is an integral part of the low pressure turbine sealing system in a demonstrator engine. Direct laser fabrication of this component fiom a bed a loose powder results in significant cost savings and improved performance over the currently employed production technique. The technology has been demonstrated by fabricating a prototype lot of 100 blade tips, which will be subjected to an engine test. This is the first instance of a direct fabrication method applied to the production of functional engine hardware. This research was funded by the United States Air Force contract F33615-94- C-2424 titled "Affordable Turbine Blade Tips".Mechanical Engineerin

Study of space shuttle environmental control and life support problems

Four problem areas were treated: (1) cargo module environmental control and life support systems; (2) space shuttle/space station interfaces; (3) thermal control considerations for payloads; and (4) feasibility of improving system reusability