Zobrazeno 1 - 10
of 34
pro vyhledávání: '"Charles H. Campbell"'
Publikováno v:
AIAA SPACE and Astronautics Forum and Exposition.
Advanced robotic and human missions to Mars require landed masses well in excess of current capabilities. One approach to safely land these large payloads on the Martian surface is to extend the propulsive capability currently required during subsoni
Autor:
Tait Pottebaum, Charles H. Campbell, Vanessa V. Aubuchon, Shann J. Rufer, Richard J. Schwartz, Thomas S. Spisz, David Gibson, C. David Mercer, Steve Kennerly, Martin N. Ross, Thomas J. Horvath, Steven Tack, Kwame Osei-Wusu, Gordon Scriven
Publikováno v:
AIAA SPACE and Astronautics Forum and Exposition.
Autor:
Phil Robinson, Edward A. Robertson, Joseph A. Garcia, Susan J. Stachowiak, David J. Kinney, Charles H. Campbell, Daniel A. Matz, John E. Theisinger, Breanna J. Johnson, Christopher J. Cerimele, Ronald R. Sostaric, Jeffrey V. Bowles
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
Current NASA Human Mars architectures require delivery of approximately 20 metric tons of cargo to the surface in a single landing. A proposed vehicle type for performing the entry, descent, and landing at Mars associated with this architecture is a
Publikováno v:
Journal of Spacecraft and Rockets. 43:1202-1215
DOI: 10.2514/1.23082 This paper describes the analysis of localized catalytic heating effects to the U.S. Space Shuttle Orbiter thermal protectionsystem.Theanalysisappliestothehigh-temperaturereusablesurfaceinsulationonthelowerfuselageand wing acreag
Publikováno v:
Journal of Spacecraft and Rockets. 33:457-462
All four Space Shuttle Orbiters, which are currently operational, have limited instrumentation packages that provide information about the aerothermodynamic environment. Heat transfer rates have been determined from the measured temperature histories
Autor:
Michael Holden, Brian Anderson, Matthew MacLean, Scott A. Berry, Charles H. Campbell, Timothy Wadhams, Karen T. Berger, Shann J. Rufer
Publikováno v:
42nd AIAA Thermophysics Conference.
In an experimental study to obtain detailed heating data over the Space Shuttle Orbiter, CUBRC has completed an extensive matrix of experiments using three distinct models and two unique hypervelocity wind tunnel facilities. This detailed data will b
Autor:
Luis A. Saucedo, Charles H. Campbell, Michael T. Garske, Karen T. Berger, Brian Anderson, Gerald R. Kinder, Ann M. Micklos
Publikováno v:
42nd AIAA Thermophysics Conference.
In support of the Boundary Layer Transition Flight Experiment (BLT FE) Project, a manufactured protuberance tile was installed on the port wing of Space Shuttle Orbiter Discovery for STS-119, STS-128, STS-131 and STS-133 as well as Space Shuttle Ende
Autor:
Karl T. Edquist, Paul W. Krasa, Charles H. Campbell, Helen H. Hwang, Robin Beck, Michael J. Wright
Publikováno v:
2011 Aerospace Conference.
Landing humans on Mars is perhaps the largest Entry, Descent and Landing challenge for this (or any) generation of NASA engineers.12 Essentially all current Mars EDL technology is based on development efforts in support of the Viking program in the 1
Autor:
Charles H. Campbell, Graham V. Candler
Publikováno v:
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.
During the STS-119 flight of Space Shuttle Discovery, two sets of surface temperature measurements were made. Under the HYTHIRM program3 quantitative thermal images of the windward side of the Orbiter with a were taken. In addition, the Boundary Laye
Autor:
Max E. Larin, Gerald R. Kinder, Joseph R. Riccio, Tien Q. Nguyen, Steven V. Del Papa, Maria V. Pulsonetti, Charles H. Campbell, Jeremiah J. Marichalar
Publikováno v:
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.
A series of tests conducted recently at the NASA JSC arc -jet test facility demonstrated that a protruding tile material can survive the exposure to the high enthalpy flows characteristic of the Space Shuttle Orbiter re-entry environments. The tests