NASA Technical Reports Server (NTRS) : Project pdf

NASA Technical Reports Server (NTRS) : Project

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A high-altitude, battery-powered, propeller-driven aircraft was designed and is being built by undergraduate students at California State University, Northridge. The aircraft will fly at an altitude of 104,000 ft at Mach 0.2 (190 ft/sec) and will be instrumented to record flight performance data, including low Reynolds number propeller and airfoil information. This project will demonstrate the feasibility of electric-powered flight in a low-density, low-temperature Earth environment that models the atmosphere of Mars. Data collected will be used to design a Mars aircraft to investigate the surface of Mars prior to manned missions. The instrumented payload and the mission profile for the high-altitude Earth flight were determined. Detailed aerodynamic and structural analyses were performed. Control, tracking, and data recording subsystems were developed. Materials were obtained and fabrication begun. The aircraft has a 32-ft wing span, a wing area of 105 sq ft, is 17.5 ft long, has a 12-in payload bay, and weighs 42 lb.

It is composed primarily of lightweight materials, including Mylar, and composite materials, including graphite/epoxy and aramid core honeycomb sandwich. Low-altitude flight testing to check guidance and control systems and to calibrate data-gathering instruments will take place this summer, followed shortly by the 104,000-ft flight

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 1/1/1991
• Year: 1991
• Book Topics/Themes: NASA Technical Reports Server (NTRS), AIRCRAFT DESIGN, FLIGHT CHARACTERISTICS, FLY BY WIRE CONTROL, PROPELLER BLADES, UNIVERSITY PROGRAM, UNMANNED SPACECRAFT, AERODYNAMIC CHARACTERISTICS, AIRCRAFT CONSTRUCTION MATERIALS, FLIGHT TESTS, LOW REYNOLDS NUMBER, MARS ATMOSPHERE, STRUCTURAL ANALYSIS

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