Zobrazeno 1 - 6
of 6
pro vyhledávání: '"David C. Purinton"'
Publikováno v:
AIAA Scitech 2019 Forum.
An aerodynamic database has been generated for use by the Orion Multi-Purpose Crew Vehicle (MPCV) Program to analyze Service Module (SM) panel jettison from the NASA SLS vehicle. The database is a combination of CFD data for the panel aerodynamic coe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc9ba8146ee9db211adcee788c349af4
https://doi.org/10.2514/6.2019-1843
https://doi.org/10.2514/6.2019-1843
Publikováno v:
52nd Aerospace Sciences Meeting.
The Aerosciences Branch (EV33) at the George C. Marshall Space Flight Center (MSFC) has been responsible for a series of wind tunnel tests on the National Aeronautics and Space Administration's (NASA) Space Launch System (SLS) vehicles. The primary p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b5ed614c4e7396a6088dc092a64ab7c9
https://doi.org/10.2514/6.2014-1256
https://doi.org/10.2514/6.2014-1256
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
The simulation of the reentry phase of booster flight encompasses challenging aerodynamics and trajectories to determine environments and recovery system deployment conditions. Unlike ascent flight, reentry is uncontrolled and may travel through a la
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d1f71be1c62296461f7265e427a8cfa9
https://doi.org/10.2514/6.2011-14
https://doi.org/10.2514/6.2011-14
Publikováno v:
38th Aerospace Sciences Meeting and Exhibit.
An extensive experimental program has been conducted to determine the aerodynamic characteristics of grenade ribbon stabilizers. While data has been acquired from vertical and horizontal wind tunnel tests, free-flight drop tests, and freeflight gun t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8f3c137a7be16aa9adba9e7f6fef6503
https://doi.org/10.2514/6.2000-270
https://doi.org/10.2514/6.2000-270
Publikováno v:
32nd Joint Propulsion Conference and Exhibit.
Small pressure perturbations in the Space Shuttle Reusable Solid Rocket Motor (RSRM) are caused by the periodic expulsion of molten aluminum oxide slag from a pool that collects in the aft end of the motor around the submerged nozzle nose during the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1386963fffc57673e8a6c0254e7e4886
https://doi.org/10.2514/6.1996-2780
https://doi.org/10.2514/6.1996-2780
Publikováno v:
31st Joint Propulsion Conference and Exhibit.
In past firings of the Reusable Solid Rocket Motor (RSRM) both static test and flight motors have shown small pressure perturbations occurring primarily between 65 and 80 seconds. A joint NASA/Thiokol team investigation concluded that the cause of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::953222c4b4078e3523264d45003f8c7d
https://doi.org/10.2514/6.1995-2724
https://doi.org/10.2514/6.1995-2724