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  • Other Sources  (1,142)
  • Air Transportation and Safety  (811)
  • Engineering (General)  (331)
  • 2015-2019  (1,142)
  • 1
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    In:  CASI
    Publication Date: 2020-01-23
    Description: The paper introduces the midpoint monitoring method for detecting cell voltage imbalance in a series string of 8 electrochemical cells. Monte Carlo analysis is performed for normal cell End of Discharge open and closed circuit voltage behavior to assess the extent to which derived guard band voltage limits will detect over discharged cells, provide false positive indication, or fail to detect over discharged cells. Forward work is proposed to refine the battery monitoring method for operational use in 28V lithium ion batteries.
    Keywords: Engineering (General)
    Type: JSC-E-DAA-TN75972 , NASA Aerospace Battery Workshop; Nov 19, 2019 - Nov 21, 2019; Huntsville, AL; United States
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  • 2
    Publication Date: 2020-01-23
    Description: Low power Stirling convertors are being developed at NASA Glenn Research Center to provide future small spacecraft with electrical power by converting heat from one or more Light Weight Radioisotope Heater Units (LWRHU). An initial design converts multiple watts of heat to one watt of electrical power output using a Stirling convertor. A variety of mission concepts have been studied by NASA and the U. S. Department of Energy that would utilize low power Radioisotope Power Systems (RPS) for probes, landers, rovers, and repeaters. These missions would contain science instruments distributed across planetary surfaces or near objects of interest where solar flux is insufficient for using solar cells. Landers could be used to provide data such as, radiation, temperature, pressure, seismic activity, and other surface measurements for planetary science and to inform future mission planners. The studies propose using fractional versions of the General Purpose Heat Source or multiple LWRHUs to heat power conversion technologies for science instruments and communication. Dynamic power systems are capable of higher conversion efficiencies, which could enable equal power using less fuel or more power using equal fuel, when compared to less efficient static power conversion technologies. Providing spacecraft with more power would decrease duty cycling of basic functions and, therefore, increase the quality and abundance of science data. Efforts to develop the concept have focused on maturation of a 1-We convertor and controller design and performance evaluation of an evacuated metal foil insulation. A proof-of-concept 1-We convertor, controller, and evacuated metal foil insulation package have been fabricated and are undergoing characterization testing. The current status, findings, and path forward for the effort are explained in this paper.
    Keywords: Engineering (General)
    Type: NASA/TM-2019-220316 , AIAA–2019–4065 , E-19731 , GRC-E-DAA-TN71841 , International Energy Conversion Engineering Conference; Aug 19, 2019 - Aug 22, 2019; Indianapolis, IN; United States
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  • 3
    Publication Date: 2020-01-22
    Description: This presentation reviews voluntary safety reports received by NASA's Aviation Safety Reporting System pertaining to Hazardous Materials.
    Keywords: Air Transportation and Safety
    Type: ARC-E-DAA-TN74687 , Aviation Safety InfoShare; Oct 30, 2019; Bellevue, WA; United States
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  • 4
    Publication Date: 2020-01-18
    Description: Cryogenic propellant storage tank self-pressurization involves complex physical phenomena which are usually analytically modelled via complex multidimensional CFD codes. Unfortunately these codes, even when modelling axisymmetric domains, may takes weeks or longer to obtain transient pressure and temperature information for relatively short periods of time (several seconds to several hours). Propellant tank storage end-to-end mission simulations can last a duration of days to weeks to months. Multi-node modelling of propellant tanks is a viable alternative to traditional CFD modelling and presents the advantage of greatly reduced run times on the order of hours and days compared to the weeks or longer for CFD codes. A multi-node model represents the fluid within the storage tank, as well as the storage tank itself, as a fluid-thermal network. This type of setup is not necessarily geometrically based. This can be accomplished using a commercial generalized fluid-thermal network code, such as SINDA/FLUINT (SF). The advantage of using a fluid-thermal network code like SF lies in its extensive ability to model the external environment of the storage tank through the graphical user interface, Thermal Desktop (TD). The total heat load into the tank may be a function of heaters and a complex radiative environment as well. Thermal Desktop may be used to address the detailed radiative environment of the tank as well as building a geometrically accurate depiction of the storage tank itself.
    Keywords: Engineering (General)
    Type: GRC-E-DAA-TN72353 , Propulsion and Energy Forum; Aug 19, 2019 - Aug 22, 2019; Indianapolis, IN; United States
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  • 5
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    In:  CASI
    Publication Date: 2020-01-18
    Description: This presentation presents an overview of NASA's Aviation Safety Reporting System including report processing metrics and outreach activities.
    Keywords: Air Transportation and Safety
    Type: ARC-E-DAA-TN75565 , International Confidential Aviation Safety Systems (ICASS); Nov 18, 2019 - Nov 19, 2019; Seol; Korea, Republic of
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  • 6
    Publication Date: 2020-01-16
    Description: The Technology Capability Level-3 (TCL3) flight tests were conducted at six different test sites located across the USA from March to May of 2018. The campaign resulted in over 830 data collection flights using 28 different aircraft and involving 20 flight crews. Flights not only varied in duration, but also in the environments and terrains over which they flew. The TCL3 tests highlighted four different types of tests: three tests focused on Communication, Navigation and Surveillance (CNS); six tests focused on Sense and Avoid (SAA) technologies; six tests focused on USS Data and Information Exchange (DAT); and five tests focused on exploring fundamental Concepts of the project (CON). This document presents data collected during the TCL3 tests that informed the operators experiencesthe quality of the unmanned aerial system (UAS) Service Supplier (USS) information that the operator was provided with, the usefulness of this information, and the usability of the automation, both while airborne and on the ground. It is intended to complement the reports written by the test sites and the quantitative reports and presentations of the UAS Traffic Management (UTM) project. With the goal of instructing what the minimum information requirements and/or best practices might be in TCL3 operations, the driving enquiry was: How do you get the information you need, when you need it, to successfully fly a UAS in UTM airspace? This enquiry touches on two requirements for displays, which are to provide adequate situation awareness (SA) and to share information through a USS. The six test sites participating in the TCL3 tests flew a subset of the 20 tests (outlined above), with most sites working on a subset of each of the four types: Communications, Navigation and Surveillance (CNS); DAT; CON; and Sense and Avoid (SAA). The, mainly qualitative, data addressed in this report was collected by the AOL (Airspace Operations Laboratory) both on-site and remotely for each test. The data consists of the contents of end-of-day debriefs, end-of-day surveys, observer notes, and flight test information, all submitted as part of the Data Management Plan (DMP).
    Keywords: Air Transportation and Safety
    Type: NASA/TM-2019-220347 , ARC-E-DAA-TN65414
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  • 7
    Publication Date: 2020-01-16
    Description: The Traffic Aware Strategic Aircrew Request (TASAR) concept applies onboard automation for the purpose of advising the pilot of route modifications that would be beneficial to the flight. Leveraging onboard computing platforms with connectivity to avionics and diverse data sources on and off the aircraft, TASAR introduces a new, powerful capability for in-flight trajectory management to the cockpit and its flight crew that is anticipated to induce a significant culture change in airspace operations. Flight crews empowered by TASAR and its derivative technologies could transform from todays flight plan followers to proactive trajectory managers, taking an initial critical step towards increasing autonomy in the airspace system. TASAR was developed as a catalyst for operational autonomy, a future vision where the responsibilities and authorities of trajectory management reside with the aircraft operator and are distributed among participating aircraft, thus fulfilling a vision dating back decades and enabling a fully scalable airspace system. This NASA Technical Paper maps TASAR to its foundational vision and traces its research and development from initial concept generation to an operational evaluation by a U.S. airline in revenue service, the final stage before technology transfer and commercialization.
    Keywords: Air Transportation and Safety
    Type: NASA/TP–2019-220432 , NF1676L-34474
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  • 8
    Publication Date: 2020-01-14
    Description: No abstract available
    Keywords: Engineering (General)
    Type: JPL-CL-16-4241 , AIAA/AAS Astrodynamics Specialist Conference; Sep 12, 2016 - Sep 15, 2016; Long Beach, CA; United States
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  • 9
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    In:  Other Sources
    Publication Date: 2020-01-13
    Description: No abstract available
    Keywords: Engineering (General)
    Type: JPL-CL-16-3857 , Chadron State and Colorado State Student Presentation; Sep 01, 2016; Chaldron, NE; United States
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  • 10
    Publication Date: 2020-01-13
    Description: No abstract available
    Keywords: Engineering (General)
    Type: JPL-CL-16-3795 , ASA - HITRAN 2016; Aug 24, 2016 - Aug 26, 2016; Reims; United States
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