Explore: Drop Tests
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Source: The Open Library
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Search results from The Open Library
1Stress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicle
By William L. Ko
“Stress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicle” Metadata:
- Title: ➤ Stress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicle
- Author: William L. Ko
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1997
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Stress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicle” Subjects and Themes:
- Subjects: ➤ Stress concentration - Finite element method - B-52 aircraft - Pylons - Hooks - Stress analysis - Drop tests - Curved beams - Flight tests - Flight testing - Airplanes - B-52 bomber - Structural design
Edition Identifiers:
- The Open Library ID: OL15498525M - OL18118708M - OL17572316M - OL18891553M - OL17125507M
- Online Computer Library Center (OCLC) ID: 39824821
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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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.
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2Final report ... for NAS8-38609 ... entitled Materials science research
By Gary L. Workman
“Final report ... for NAS8-38609 ... entitled Materials science research” Metadata:
- Title: ➤ Final report ... for NAS8-38609 ... entitled Materials science research
- Author: Gary L. Workman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Final report ... for NAS8-38609 ... entitled Materials science research” Subjects and Themes:
- Subjects: Containerless melts - Drop tests - Space processing - Binary alloys - Weightlessness simulation
Edition Identifiers:
- The Open Library ID: OL18133106M - OL17597194M - OL15543416M - OL17129057M
- Online Computer Library Center (OCLC) ID: 40899341
Access and General Info:
- First Year Published: 1996
- 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.
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3Crashworthy evaluation of a 1/5-scale model composite fuselage concept
By Karen E. Jackson
“Crashworthy evaluation of a 1/5-scale model composite fuselage concept” Metadata:
- Title: ➤ Crashworthy evaluation of a 1/5-scale model composite fuselage concept
- Author: Karen E. Jackson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: [Springfield, Va - Hampton, Va
“Crashworthy evaluation of a 1/5-scale model composite fuselage concept” Subjects and Themes:
- Subjects: ➤ Applications programs (Computers) - Composite materials - Crashes - Crashworthiness - Drop tests - Finite element method - Fuselages - Impact tests - Scale models - Structural reliability
Edition Identifiers:
- The Open Library ID: OL17135402M - OL17701300M - OL17591912M
- Online Computer Library Center (OCLC) ID: 42758525
Access and General Info:
- First Year Published: 1999
- 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.
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4Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
By Matthew Robert Whiting
“Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail” Metadata:
- Title: ➤ Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
- Author: Matthew Robert Whiting
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail” Subjects and Themes:
- Subjects: ➤ X-31 - Canard configurations - Directional control - Wind tunnel tests - Drop tests - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15423353M - OL17796404M
- Online Computer Library Center (OCLC) ID: 35270882
Access and General Info:
- First Year Published: 1996
- 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.
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5Influence of temperature and impact velocity on the coefficient of restitution
By Kevin C. Radil
“Influence of temperature and impact velocity on the coefficient of restitution” Metadata:
- Title: ➤ Influence of temperature and impact velocity on the coefficient of restitution
- Author: Kevin C. Radil
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Influence of temperature and impact velocity on the coefficient of restitution” Subjects and Themes:
- Subjects: ➤ Balls - Energy absorption - Velocity measurements - Cryogenic temperature - Impact tests - Temperature effects - Atmospheric temperature - Vibration damping - Drop tests - Coefficients
Edition Identifiers:
- The Open Library ID: OL17790366M - OL15404494M
- Online Computer Library Center (OCLC) ID: 32320711
Access and General Info:
- First Year Published: 1994
- 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.
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6Muscle feasibility for cosmos rhesus
By V. Reggie Edgerton
“Muscle feasibility for cosmos rhesus” Metadata:
- Title: ➤ Muscle feasibility for cosmos rhesus
- Author: V. Reggie Edgerton
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Muscle feasibility for cosmos rhesus” Subjects and Themes:
- Subjects: ➤ Drop tests - Electromyography - Exercise physiology - Locomotion - Monkeys - Muscles - Posture - Psychomotor Performance
Edition Identifiers:
- The Open Library ID: OL15506260M
Access and General Info:
- First Year Published: 1994
- 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.
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7Lateral stability analysis for X-29A drop model using system identification methodology
By David L. Raney
“Lateral stability analysis for X-29A drop model using system identification methodology” Metadata:
- Title: ➤ Lateral stability analysis for X-29A drop model using system identification methodology
- Author: David L. Raney
- Language: English
- Number of Pages: Median: 24
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Lateral stability analysis for X-29A drop model using system identification methodology” Subjects and Themes:
- Subjects: ➤ Aircraft models - Directional stability - Drop tests - Flight characteristics - Flight stability tests - Grumman X-29A (Jet plane) - Lateral Stability of airplanes - Lateral stability - Measurement - Stability of airplanes, Lateral - Swept forward wings - System identification - X-29 aircraft
Edition Identifiers:
- The Open Library ID: OL17683289M
Access and General Info:
- First Year Published: 1989
- 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.
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8Research relative to the development of a cryogenic microwave cavity gradiometer for orbital use
By Mario D. Grossi
“Research relative to the development of a cryogenic microwave cavity gradiometer for orbital use” Metadata:
- Title: ➤ Research relative to the development of a cryogenic microwave cavity gradiometer for orbital use
- Author: Mario D. Grossi
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Goddard Space Flight Center - Smithsonian Institution, Astrophysical Observatory
- Publish Date: 1984
- Publish Location: ➤ Cambridge, Mass - Greenbelt, Md
“Research relative to the development of a cryogenic microwave cavity gradiometer for orbital use” Subjects and Themes:
- Subjects: ➤ Cavity resonators - Microwave tubes - Gravity gradiometers - Planetary gravitation - Space vehicles - Satellite instruments - Drop tests - Free fall - Attitude control systems
Edition Identifiers:
- The Open Library ID: OL16157256M
Access and General Info:
- First Year Published: 1984
- 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.
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