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Design of a Mars Airplane Propulsion System for the Aerial Regional-Scale Environmental Survey (ARES) Mission Concept

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Design of a Mars Airplane Propulsion System for the Aerial Regional-Scale Environmental Survey (ARES) Mission Concept https://ntrs.nasa.gov/search.jsp?R=20090013211 2019-08-30T06:27:23+00:00Z NASA/TM-2009-215700 Design of a Mars Airplane Propulsion System for the Aerial Regional-Scale Environmental Survey (ARES) Mission Concept Christopher A. Kuhl Langley Research Center, Hampton, Virginia March 2009 NASA STI Program . in Profile Since its founding, NASA has been dedicated to • CONFERENCE PUBLICATION. Collected the advancement of aeronautics and space science. papers from scientific and technical The NASA scientific and technical information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or co-sponsored by NASA. this important role. • SPECIAL PUBLICATION. Scientific, The NASA STI program operates under the technical, or historical information from NASA auspices of the Agency Chief Information Officer. It programs, projects, and missions, often collects, organizes, provides for archiving, and concerned with subjects having substantial disseminates NASA’s STI. The NASA STI program public interest. provides access to the NASA Aeronautics and Space Database and its public interface, the NASA Technical • TECHNICAL TRANSLATION. English- Report Server, thus providing one of the largest language translations of foreign scientific and collections of aeronautical and space science STI in technical material pertinent to NASA’s mission. the world. Results are published in both non-NASA channels and by NASA in the NASA STI Report Specialized services also include creating custom Series, which includes the following report types: thesauri, building customized databases, and organizing and publishing research results. • TECHNICAL PUBLICATION. Reports of completed research or a major significant phase For more information about the NASA STI of research that present the results of NASA program, see the following: programs and include extensive data or theoretical analysis. Includes compilations of • Access the NASA STI program home page at significant scientific and technical data and http://www.sti.nasa.gov information deemed to be of continuing reference value. NASA counterpart of peer- • E-mail your question via the Internet to reviewed formal professional papers, but having [email protected] less stringent limitations on manuscript length and extent of graphic presentations. • Fax your question to the NASA STI Help Desk at 443-757-5803 • TECHNICAL MEMORANDUM. Scientific and technical findings that are preliminary or of • Phone the NASA STI Help Desk at specialized interest, e.g., quick release reports, 443-757-5802 working papers, and bibliographies that contain minimal annotation. Does not contain extensive • Write to: analysis. NASA STI Help Desk NASA Center for AeroSpace Information • CONTRACTOR REPORT. Scientific and 7115 Standard Drive technical findings by NASA-sponsored Hanover, MD 21076-1320 contractors and grantees. NASA/TM-2009-215700 Design of a Mars Airplane Propulsion System for the Aerial Regional-Scale Environmental Survey (ARES) Mission Concept Christopher A. Kuhl Langley Research Center, Hampton, Virginia National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 March 2009 Trade names and trademarks are used in this report for identification only. Their usage does not constitute an official endorsement, either expressed or implied, by the National Aeronautics and Space Administration. Available from: NASA Center for AeroSpace Information 7115 Standard Drive Hanover, MD 21076-1320 443-757-5802 TABLE OF CONTENTS 1.0 Introduction .................................................................................................................................................3 2.0 Mission Description.....................................................................................................................................3 2.1 Concept of Operations ..............................................................................................................................3 2.2 Target Region............................................................................................................................................4 2.3 Atmospheric Flight System (Airplane) .....................................................................................................5 3.0 Propulsion Subsystem Trade Studies ........................................................................................................6 3.1 Propeller Development .............................................................................................................................6 3.2 Electrical Propulsion Systems...................................................................................................................6 3.3 Combustion Engine Systems.....................................................................................................................7 3.4 Rocket Systems.........................................................................................................................................7 3.5 Airplane Propulsion Subystem Selection..................................................................................................8 4.0 Bipropellant Rocket Subsystem Design.....................................................................................................9 4.1 System Schematic and Layout ..................................................................................................................9 4.2 High Pressure Helium Storage Tank.......................................................................................................12 4.3 Propellant Tanks .....................................................................................................................................12 4.3.1 Tank Design........................................................................................................................................12 4.3.2 Propellant Management Device (PMD) Design .................................................................................13 4.4 Bipropellant Thrusters.............................................................................................................................15 4.4.1 22N Satellite Reaction Control Thruster Options...............................................................................15 4.4.2 AMPAC-ISP 22-N Columbium Thruster ...........................................................................................16 4.4.3 Thruster Mounting and Orientation ....................................................................................................17 4.5 Thruster Valves.......................................................................................................................................18 4.6 Propellant Isolation and Flow Control Hardware ...................................................................................19 4.6.1 Pyrotechnic-actuated Valves (Pyrovalves) .........................................................................................19 4.6.2 Line Filters..........................................................................................................................................19 4.6.3 Check Valves......................................................................................................................................19 4.6.4 Helium Regulator................................................................................................................................20 4.6.5 Flow Venturis .....................................................................................................................................20 4.6.6 Service Valves ....................................................................................................................................20 4.6.7 Fluid Field Joints ................................................................................................................................20 4.7 Command and Instrumentation...............................................................................................................20 4.7.1 Temperature Sensors ..........................................................................................................................21 4.7.2 Pressure Transducer............................................................................................................................21 4.8 Hardware Integration ..............................................................................................................................22 5.0 Master Equipment List .............................................................................................................................23 6.0 Propulsion Subsystem Performance........................................................................................................24 6.1 Thruster Firing – Thermal Impact...........................................................................................................24 6.2 Thruster Plumes ......................................................................................................................................26 6.3 Thruster Firing Logic..............................................................................................................................27 6.4 Airplane Flight Simulation......................................................................................................................27 6.5 Airplane Flight Duration and
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