Explore: Ducted Rocket Engines
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Cold-flow study of low frequency pressure instability in hybrid rocket motors
By Rhonald M. Jenkins
“Cold-flow study of low frequency pressure instability in hybrid rocket motors” Metadata:
- Title: ➤ Cold-flow study of low frequency pressure instability in hybrid rocket motors
- Author: Rhonald M. Jenkins
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Cold-flow study of low frequency pressure instability in hybrid rocket motors” Subjects and Themes:
- Subjects: ➤ Flow velocity - Ducted rocket engines - Flow visualization - Two dimensional flow - Hybrid propulsion - Heat of combustion - Rocket engines
Edition Identifiers:
- The Open Library ID: OL17126467M - OL18121641M - OL17837328M - OL15505680M
- Online Computer Library Center (OCLC) ID: 40196419
Access and General Info:
- First Year Published: 1997
- 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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2Experimental and analytical methods for the determination of connected-pipe ramjet and ducted rocket internal performance
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Experimental and analytical methods for the determination of connected-pipe ramjet and ducted rocket internal performance” Metadata:
- Title: ➤ Experimental and analytical methods for the determination of connected-pipe ramjet and ducted rocket internal performance
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Number of Pages: Median: 103
- Publisher: AGARD
- Publish Date: 1994
- Publish Location: Neuilly sur Seine, France
“Experimental and analytical methods for the determination of connected-pipe ramjet and ducted rocket internal performance” Subjects and Themes:
- Subjects: Ducted rocket engines - Ramjet engines
Edition Identifiers:
- The Open Library ID: OL22347154M
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.
Online Borrowing:
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3Final report on fundamental phenomena on fuel decomposition and boundary-layer combustion precesses with applications to hybrid rocket motors
By Kenneth K. Kuo and C. L. Merkle
“Final report on fundamental phenomena on fuel decomposition and boundary-layer combustion precesses with applications to hybrid rocket motors” Metadata:
- Title: ➤ Final report on fundamental phenomena on fuel decomposition and boundary-layer combustion precesses with applications to hybrid rocket motors
- Authors: Kenneth K. KuoC. L. Merkle
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Penn State - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va - University Park, Pa
“Final report on fundamental phenomena on fuel decomposition and boundary-layer combustion precesses with applications to hybrid rocket motors” Subjects and Themes:
- Subjects: ➤ Combustion physics - Fuel combustion - Boundary layers - Ducted rocket engines - Hybrid rocket engines - Propulsion system performance
Edition Identifiers:
- The Open Library ID: OL17837087M
- Online Computer Library Center (OCLC) ID: 39892763
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.
Online Borrowing:
Online Marketplaces
Find Final report on fundamental phenomena on fuel decomposition and boundary-layer combustion precesses with applications to hybrid rocket motors at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Rocket engine
man-sized weapons to huge spaceships. Compared to other types of jet engine, rocket engines are the lightest and have the highest thrust, but are the least
Air-augmented rocket
known as ducted rockets or shrouded rockets depending on the details of the expander. In a conventional chemical rocket engine, the rocket carries both
Ramjet
increases total pressure recovery. In a throttleable ducted rocket, also known as a variable flow ducted rocket, a valve allows the gas generator exhaust to be
Jet engine
closely remember the ducted fan blades of turbofan engines. Propfans are designed to offer the speed and performance of turbofan engines with fuel efficiency
Rocket-based combined cycle
and ducted rocket, where all three systems use a shared flow path. A TBCC, or turbine-based combined cycle propulsion system, is a turbine engine combined
Aircraft engine
as powered flight. Most aircraft engines are either piston engines or gas turbines, although a few have been rocket powered and in recent years many small
RS-25
increased by two solid rocket boosters and the orbiter's two AJ10 orbital maneuvering system engines. Following each flight, the RS-25 engines were removed from
Airbreathing jet engine
An airbreathing jet engine (or ducted jet engine) is a jet engine in which the exhaust gas which supplies jet propulsion is atmospheric air, which is
Rocket-powered aircraft
A rocket-powered aircraft or rocket plane is an aircraft that uses a rocket engine for propulsion, sometimes in addition to airbreathing jet engines. Rocket
Solid Fuel Ducted Ramjet
missiles. The Solid Fuel Ducted Ramjet (SFDR) is a missile propulsion system that includes a thrust modulated ducted rocket with a reduced smoke nozzle-less