A Densified Liquid Methane Delivery System for the Altair Ascent StageA Densified Liquid Methane Delivery System for the Altair Ascent Stage download pdf

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Author: National Aeronautics and Space Adm Nasa
Published Date: 14 Jan 2019
Publisher: Independently Published
Language: English
Book Format: Paperback::40 pages
ISBN10: 179395481X
ISBN13: 9781793954817
Filename: a-densified-liquid-methane-delivery-system-for-the-altair-ascent-stage.pdf
Dimension: 216x 279x 2mm::118g
Download: A Densified Liquid Methane Delivery System for the Altair Ascent Stage
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A Densified Liquid Methane Delivery System for the Altair Ascent Stage download pdf. In a Phase I Development Program test, the CECE demonstrated an overall deep The Exploration Systems Mission Directorate is expected to use and refine some of allowing the cushioned shipping containers to fall directly onto the surface. Liquid Oxygen Liquid Methane Lunar ascent main engine CASI: A01, Hardcopy The liquid-oxygen (LO2)/methane propellant combination has been baselined for the Lunar Surface Access Module ascent engine main propulsion. The proposed switch from the hypergolic propellants used in the Apollo lunar ascent engine to LO2/methane propellants requires the development of igniters capable of highly reliable performance in a lunar surface environment. The Altair Lunar Lander is currently carrying options for both cryogenic and hypergolic ascent stage propulsion modules. The cryogenic option uses liquid American Institute of Aeronautics and Astronautics 12700 Sunrise Valley Drive, Suite 200 Reston, VA 20191-5807 703.264.7500 The vehicle was assumed to be the Mars Ascent Vehicle (MAV) first stage tanks (shown in Fig. 2).The liquid oxygen tank surface area is 19.4 m 2 (of which 10.4 m 2 sees the Mars Atmosphere and 9 m 2 sees the methane tank) and has a volume of 7.9 m 3.The tanks have a nominal heat load of 88 W with no margin. W.L. Johnson, T.M. TomsikA densified liquid methane delivery system for the Altair ascent stage The SpaceOps 2010 Conference, AIAA, Reston, VA (2010) Google Scholar The Sheahan Diamond Literature Reference Compilation; The Sheahan Diamond Literature Reference Compilation is compiled Patricia Sheahan. Who publishes on a monthly basis a list of new scientific articles related to diamonds as well as media coverage and corporate announcementscalled the Sheahan Diamond Literature Service that is distributed as a free pdf to a list of followers. Pat has kindly agreed Get this from a library! A densified liquid methane delivery system for the Altair ascent stage. [Thomas M Tomsik; NASA Glenn Research Center.; American Institute of Aeronautics and Astronautics.;] Buy A Densified Liquid Methane Delivery System for the Altair Ascent Stage on FREE SHIPPING on qualified orders This document includes two NASA program solicitations with separate research areas under which small business concerns (SBCs) are invited to submit proposals: the Small Business Innovation Research (SBIR) program and the Small Business Technology Transfer (STTR) program. Program background information, eligibility requirements for participants Exploration Systems Architecture Study conducted NASA in 2005 identified the liquid oxygen (LOx)/ liquid methane (LCH4) propellant combination as a prime candidate for the Crew Exploration Vehicle Service Module propulsion and for later use for ascent stage propulsion of the lunar lander. Both the Crew Exploration Vehicle and Lunar Lander were part the Constellation architecture, which had the objective A Densified Liquid Methane Delivery System for the Altair Ascent Stage. Wesley Johnson, Thomas Tomsik, Todd Smudde, Andrew Schnell and Mark Femminineo; Wesley Johnson. NASA Kennedy Space Center. Search for more papers this author,Thomas Tomsik. NASA Glenn Research Center. Search for more papers this author,Todd Smudde. NASA Kennedy Space Center. Search for more papers There is increasing interest in developing biobased alternative jet fuels to meet rising aviation demand and address environmental concerns. Uncertainty of oil prices, issues of energy security, and rising greenhouse gas concentrations have spurred the development and acceptance of alternative, economically viable, environmentally sustainable production pathways. The objectives of this study [4]TOMSIK T. Performance tests of a liquid hydrogen propellant densification ground system for the X33/RLV [C] The 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit. Reston, VA, USA: AIAA, 1997: 117. A Densified Liquid Methane Delivery System for the Altair Ascent Stage219 Wesley Johnson, Thomas Tomsik, Todd Smudde, Andrew Schnell, Mark Femminineo Functional Fault Modeling Conventions and Practices for Real-Time Fault Isolation NASA's communications capability is based on the premise that communications shall enable and not constrain missions. Communications must be robust to support the numerous mission Liquid Oxygen / Liquid Methane Test Results of the RS-18 Lunar Ascent Engine at Simulated Altitude Conditions at NASA White Sands Test Facility A Densified Liquid Methane Delivery System for the Altair Ascent Stage. NASA Technical Reports Server (NTRS) Tomsik, Thomas M.; Johnson, Wesley L.; Smudde, Todd D.; Femminineo, Mark F.; Schnell, Andrew R. 2010-01-01.The Altair Lunar Lander is currently carrying options for both cryogenic and hypergolic ascent stage propulsion modules. The cryogenic option uses liquid methane and liquid oxygen to A densified liquid methane delivery system for the Altair ascent stage; A design of a modular GPHS-Stirling power system for a Lunar habitation module; A dual-plane PIV study of turbulent heat transfer flows; A full-text-based search engine for finding highly matched documents across multiple categories Modeling the RL10 with Densified Liquid Hydrogen and Oxygen Propellants. Mark Haberbusch, Antony Skaff, Chinh Nguyen and Laurie Walls; 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit June 2012. Thermodynamic models for investigating environmental heating effects on densified propellants for ELVs. Mark Haberbusch and Michael Meyer; 36th AIAA/ASME/SAE/ASEE Joint The Altair Lunar Lander is currently carrying options for both cryogenic and hypergolic ascent stage propulsion modules. The cryogenic option uses liquid methane and liquid oxygen to propel Altair Complete award history of NASA's SBIR/STTR program from 1984 till present that would help to get an understanding of what has been funded 9780309082693 0309082692 Evaluation of Alternative Technologies for Disposal of Liquid Wastes from the Explosive Destruction System, Committee on Review and Evaluation of the Army Non-Stockpile Chemical Material Disposal Program, Board on Army Science and Technology, Division on Engineering and Physical Sciences, Cryogenic Fluid Technologies for Long Duration In-Space Operations Susan M. Motil/NASA Glenn Research Center Terri L. Tramel/NASA Marshall Space Flight Center Reliable knowledge of low-gravity cryogenic fluid management behavior is lacking and yet is critical in the areas of storage, distribution, and low-gravity propellant management. The Vision for Space Exploration mission objectives will require Because it uses liquid hydrogen, it's very tall and therefore needs a And sure, they showed an ascent stage on top of it, but that appears to be provided NASA. 4) Altair. At least they were trying for more capability than Apollo. Less payload, but the Soviets did a fine job systems engineering a clever NASA Historical Data Book 1989-1998 - Free ebook download as PDF File (.pdf), Text File (.txt) or read book online for free. NASA Historical Data Book 1989-1998. Official NASA data on manned and unmanned projects. Launch dates, durations, landing times, weights, etc. Published NASA in 2009. Description: It's not a new home brewing system, the world's largest holiday tank is an important component of testing for the Altair lunar lander, an Determining how liquid methane would react to being stored on the moon Small Business Technology Transfer (STTR) program. Program background information, eligibility requirements for participants, the three program phases, and information for submitting responsive proposals is contained herein. The 2009 Solicitation period for Phase 1 proposals begins July 7, 2009, and ends September 3, 2009. The mission goals of the EOS program were to 1) create an integrated, scientific observing system emphasizing climate change that would enable multidisciplinary studies of Earth s critical, interrelated processes; 2) develop a comprehensive data information system, including a data retrieval and processing system; 3) serve the needs of scientists performing an integrated multidisciplinary study of Extensive modifications were made to the test facility s existing liquid hydrogen system for compatibility with liquid methane. Also, a new liquid methane fluid conditioning system will enable liquid methane to be quickly densified (sub-cooled below normal boiling point) and to be quickly reheated to saturation conditions between 92 and 140 K A Densified Liquid Methane Delivery System for the Altair Ascent Stage Thomas M. Tomsik National Aeronautics and Space Administration Glenn Research Center Cleveland, Ohio 44135 Wesley L. Johnson, Todd D. Smudde, and Mark F. Femminineo National Aeronautics and Space Administration Kennedy Space Center Kennedy Space Center, Florida 32899 Andrew An approved accounting system can track costs to final cost objectives and segregate costs between direct and indirect. If you currently do not have an adequate accounting system, it is recommended that you take action to implement such a system. The lack of an adequate accounting system may preclude you from receiving a Phase 2 contract or may It's not a new home brewing system, the world's largest holiday ornament or tank is an important component of testing for the Altair lunar lander, an filled with liquid methane and extensively tested in a simulated lunar Exploration Systems Architecture Study conducted NASA in 2005 identified the liquid oxygen (LOx)/ liquid methane (LCH4) propellant combination as a prime candidate for the Crew Exploration Vehicle Service Module propulsion and for later use for ascent stage propulsion of the lunar lander. Both the Crew Exploration Vehicle and Lunar Lander were part the Constellation architecture,

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