Design, Fabrication, and Testing of a Cesium Ion Rocket Engine
Quarterly Progress Report No.2: December 1st 1960 through February 28 1961
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Quarterly Progress Report No.2: December 1st 1960 through February 28 1961
Structural design, analysis, and testing procedures in construction and evaluation of Mariner I space probe
Conference on reduction and suppression of aircraft engine noise
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R-4D engine attitude control and performance under launch and space stresses
NASA/GE Power Extraction Demonstration Summary Presentation for Turbine Engine Technology Symposium (TETS) 2026.
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Basic periods in the history of the development of ramjet engine theory are cited. The periods include the first experimental tests as well as the development of basic ideas and theoretical development of the cosmic ramjet engine.
Changes in engine technology such as higher temperatures, higher tip speeds, new metal/composite/ceramic materials together with radical changes in design philosophy will require amongst other prerequisites the ability to measure and to monitor key internal gas and structural characteristics. The symposium papers presented non-intrusive measurement and analysis technologies in the following categories: Laser Point Measurements (11); Absorption and Infrared Techniques (4); Paints - Surface Sensors (6); Laser Induced Fluorescence (6); Mechanical (7); Films (5); Laser Planar Measurement (9); and a Keynote Address.
This report provides a regulatory gap assessment of the Federal Aviation Administration (FAA) and the European Union Aviation Safety Agency (EASA) Special Conditions (SC) for electric engines. This information is presented to support ongoing international harmonization efforts for electric engine certification, to establish a level of safety consistent across regulatory bodies and equivalent to that of existing combustion engines. HS Advanced Concepts LLC assembled a team of subject-matter experts to develop a comprehensive comparison of the regulatory text of EASA SC E-19 and the FAA special conditions for the certification of electric engines. The team included Mr. Chris Baczynski of BAC Aerospace Inc. and Mr. Zach Kaufman, formerly with magniX.
Abstract not provided.
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Atomic and molecular layer deposition (ALD and MLD) are two promising tools for practicing interface engineering of lithium metal anodes precisely.
This project, conducted by TDA Research, Inc. in collaboration with GE Research under DOE Award DE-FE0032261, developed and demonstrated advanced structured sorbent-coated contactors for the high-performance Direct Air Capture (DAC) of CO 2 .
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By employing 3,5-bis(trifluoromethyl) pyrazole (TFMP) as an electrolyte additive in both aqueous and non-aqueous mediums, a versatile interphase strategy is achieved. This facilitates stable Zn anodes with improved efficiency and longer cycling life.