Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Peter F. Covell"'
Autor:
Scott D. Holland, Jeremy T. Pinier, Peter F. Covell, Bandu N. Pamadi, Jing Pei, Goetz H. Klopfer
Publikováno v:
Journal of Spacecraft and Rockets. 49:864-874
Autor:
Noah M. Favaregh, Bandu N. Pamadi, Jing Pei, Peter F. Covell, Clyde R. Gumbert, Jeremy L. Hanke
Publikováno v:
Journal of Spacecraft and Rockets. 49:586-595
NASA Langley Research Center, in partnership with NASA Marshall Space Flight Center and NASA Ames Research Center, was involved in the aerodynamic analysis, testing, and database development for the Ares I A106 crew launch vehicle in support of the A
Autor:
Bandu N. Pamadi, Thomas A. Neirynck, Nathaniel J. Hotchko, William I. Scallion, Kelly J. Murphy, Peter F. Covell
Publikováno v:
Journal of Spacecraft and Rockets. 44:66-80
Autor:
Noah M. Favaregh, Bandu N. Pamadi, Clyde R. Gumbert, Jeremy L. Hanke, Jing Pei, Peter F. Covell
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
NASA Langley Research Center, in partnership with NASA Marshall Space Flight Center and NASA Ames Research Center, was involved in the aerodynamic analyses, testing, and database development for the Ares I A106 crew launch vehicle in support of the A
Autor:
Jeremy T. Pinier, Scott D. Holland, Klopfer, Goetz, H., Peter F. Covell, Jing Pei, Bandu N. Pamadi
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
This paper presents the aerodynamic analysis and database development for the first stage separation of the Ares I A106 Crew Launch Vehicle configuration. Separate databases were created for the first stage and upper stage. Each database consists of
Publikováno v:
Journal of Aircraft. 28:683-688
An Euler code study has been conducted on a transatmospheric vehicle at Mach numbers from 1.5-4.5. The results show that the Euler code accurately predicted the lift, drag, and pitching-moment coefficients as a function of Mach number and angle of at
Autor:
Bandu N. Pamadi, Jamshid A. Samareh, Nathaniel J. Hotchko, Peter F. Covell, Paul V. Tartabini
Publikováno v:
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference.
The development of methodologies, techniques, and tools for analysis and simulation of multi-body separation is critically needed for successful design and operation of next generation launch vehicles. As a part of this activity, ConSep simulation to
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference and Exhibit.
NASA has initiated a comprehensive stage separation tool development activity to address the technology needed for successful development and operation of next generation reusable launch vehicles. As a part of this activity, ConSep simulation tool is
Publikováno v:
22nd Applied Aerodynamics Conference and Exhibit.
NASA-Langley Research Center is conducting system level studies on an-house concept of a small launch vehicle to address NASA's needs for rapid deployment of small payloads to Low Earth Orbit. The vehicle concept is a three-stage system with a reusab
Publikováno v:
Aircraft Design, Systems and Operations Conference.
The NASA-Langley AST31 high-speed civil transport (HSCT) configuration, a blended wing/fuselage concept scaled for 250-passenger carriage over 6500 nmi, has been subjected to both CFD and wind tunnel tests; the wind tunnel tests were conducted in the