Explore: Aeroshells
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AI-Generated Overview About “aeroshells”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
By Ramadas K. Prabhu
“An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5” Metadata:
- Title: ➤ An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5” Subjects and Themes:
- Subjects: ➤ Aeroshells - Computational fluid dynamics - Mars missions - Aerodynamics - Wind tunnel tests - Inviscid flow - Aerodynamic characteristics - Mach number
Edition Identifiers:
- The Open Library ID: OL17719832M - OL17621409M
- Online Computer Library Center (OCLC) ID: 54502386
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
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2Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
By Ramadas K. Prabhu
“Inviscid flow computations of several aeroshell configurations for a '07 Mars lander” Metadata:
- Title: ➤ Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Inviscid flow computations of several aeroshell configurations for a '07 Mars lander” Subjects and Themes:
- Subjects: Aeroshells - Inviscid flow - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17607400M - OL17718835M
- Online Computer Library Center (OCLC) ID: 50120009
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Inviscid flow computations of several aeroshell configurations for a '07 Mars lander at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
By Ramadas K. Prabhu
“Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24” Metadata:
- Title: ➤ Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24” Subjects and Themes:
- Subjects: Computational fluid dynamics - Inviscid flow - Aeroshells - Spacecraft structures
Edition Identifiers:
- The Open Library ID: OL16030675M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Superalloy foams for aeroshell applications
By John Gayuda
“Superalloy foams for aeroshell applications” Metadata:
- Title: ➤ Superalloy foams for aeroshell applications
- Author: John Gayuda
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: Cleveland, Ohio - Hanover MD
“Superalloy foams for aeroshell applications” Subjects and Themes:
- Subjects: Aeroshells - Metal foams - Thermal protection - Heat resistant alloys - Characterization
Edition Identifiers:
- The Open Library ID: OL16037103M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Superalloy foams for aeroshell applications at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Aeroshell
dynamics of aeroshells are influenced by inertial and drag forces, as defined it this equation: ß=m/CdA where m is defined as the mass of the aeroshell and its
Pioneer Venus project
targeted at different parts of the planet; They had no parachutes and the aeroshells did not separate from the probe. Two of the small probes reached the surface
Atmospheric entry
Pathfinder and Mars Exploration Rover (MER) aeroshells. The BIP was at the attachment points between the aeroshell's backshell (also called the afterbody or
Voyager program (Mars)
landers would have been Surveyor moon probes modified with the use of aeroshells and a combination parachute/retrorocket landing systems. Funding for the
Aerocapture
and atmospheric guidance techniques have shown that heritage low-L/D aeroshells such as Apollo offer sufficient control authority for aerocapture at Neptune
Mars Exploration Rover
Colorado, the aeroshell is made of an aluminium honeycomb structure sandwiched between graphite-epoxy face sheets. The outside of the aeroshell is covered
Alaska Airlines Flight 261
manufacturer McDonnell Douglas) of Aeroshell 33 grease instead of the previously approved lubricant, Mobilgrease 28. The use of Aeroshell 33 was found not to be a
Crack the Skye
we've previously recorded in the sense that we kinda strapped on our aeroshells and departed from Earth for a while, and then captained to the ethereal
Viking program
above the surface by the extended legs. Each lander was enclosed in an aeroshell heat shield designed to slow the lander down during the entry phase. To
EAA AirVenture Oshkosh
Aeroshell Aerobatic Team performing at EAA AirVenture 2007