AGARD-AR-350

AGARD-AR-350
  • Version
  • 392 Downloads
  • 32.74 MB File Size
  • 1 File Count
  • April 25, 2016 Create Date
  • April 25, 2016 Last Updated
Scroll for Details

Structural Assessment of Solid Propellant Grains
AGARD-AR-350 Structural Assessment of Solid Propellant Grains
The recorded use of solid propellant rockets in battle spans many centuries. Today the solid propellant
rocket maintains a prominent position supplying propulsion for a wide range of missiles. Numerous
systems are in service or development and the future of solid propellant rockets seems assured well into
the next century. The capability to design, develop and manufacture solid propellant rockets is spread
widely across the NATO countries and the trend is for these technologies to become yet more
widespread.
Solid propellant rocket motors are the primary propulsion choice for short and medium range missiles.
Even the growing interest in ramjet and ramrocket propulsion technology required for the longer range
applications carries with it the need for a solid propellant boost motor to accelerate the missile to a
velocity sufficient to sustain the airbreathing mode.
Within the overall matrix of solid propellant rocket motor technologies, grain structural integrity
remains a challenging area for design engineers. It is a key discipline that governs performance,
reliability and service life. The environments in which rocket motors are asked to operate are becoming
more and more severe, particularly for air-carried missiles where low and high temperature extremes
are experienced. The ability to predict and verify adequate structural margins for such systems is vital.
The technical problems are common for all workers in the field. However, the analysis methods
employed, and the design standards required, differ from one country to another and even from
company to company within the same country. This lack of standardisation presents problems when
assessing foreign design proposals, when participating in multinational projects, and in the ownership
of foreign missile systems where safety and serviceability need to be monitored. The growing pressure
for longer service life compounds the problem. There is a clear need for knowledge and understanding
of the methods, standards and criteria used in each NATO country.

FileAction
AGARD-AR-350 Structural Assessment of Solid Propellant Grains.pdfDownload 

Comment On This Post

Your email address will not be published. Required fields are marked *

AGARD-AR-350

AGARD-AR-350
  • Version
  • 392 Downloads
  • 32.74 MB File Size
  • 1 File Count
  • April 25, 2016 Create Date
  • April 25, 2016 Last Updated
Scroll for Details

Structural Assessment of Solid Propellant Grains
AGARD-AR-350 Structural Assessment of Solid Propellant Grains
The recorded use of solid propellant rockets in battle spans many centuries. Today the solid propellant
rocket maintains a prominent position supplying propulsion for a wide range of missiles. Numerous
systems are in service or development and the future of solid propellant rockets seems assured well into
the next century. The capability to design, develop and manufacture solid propellant rockets is spread
widely across the NATO countries and the trend is for these technologies to become yet more
widespread.
Solid propellant rocket motors are the primary propulsion choice for short and medium range missiles.
Even the growing interest in ramjet and ramrocket propulsion technology required for the longer range
applications carries with it the need for a solid propellant boost motor to accelerate the missile to a
velocity sufficient to sustain the airbreathing mode.
Within the overall matrix of solid propellant rocket motor technologies, grain structural integrity
remains a challenging area for design engineers. It is a key discipline that governs performance,
reliability and service life. The environments in which rocket motors are asked to operate are becoming
more and more severe, particularly for air-carried missiles where low and high temperature extremes
are experienced. The ability to predict and verify adequate structural margins for such systems is vital.
The technical problems are common for all workers in the field. However, the analysis methods
employed, and the design standards required, differ from one country to another and even from
company to company within the same country. This lack of standardisation presents problems when
assessing foreign design proposals, when participating in multinational projects, and in the ownership
of foreign missile systems where safety and serviceability need to be monitored. The growing pressure
for longer service life compounds the problem. There is a clear need for knowledge and understanding
of the methods, standards and criteria used in each NATO country.

FileAction
AGARD-AR-350 Structural Assessment of Solid Propellant Grains.pdfDownload 
17,005 Documents in our Technical Library
2653909 Total Downloads

Search The Technical Library

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...