Fragmentation data was assembled and analyzed for exploding liquid propellant vessels. These data were to be retrieved from reports of tests and accidents, including measurements or estimates of blast yield, etc. A significant amount of data was retrieved from a series of tests conducted for measurement of blast and fireball effects of liquid propellant explosions (Project PYRO), a few well-documented accident reports, and a series of tests to determine auto-ignition properties of mixing liquid propellants. The data were reduced and fitted to various statistical functions. Comparisons were made with methods of prediction for blast yield, initial fragment velocities, and fragment range. Reasonably good correlation was achieved. Methods prese...
NASA is developing launch vehicles to support missions to Low Earth Orbit (LEO), the moon and deep s...
Data and theory pertinent to the autoignition of liquid oxygen/liquid hydrogen and liquid oxygen pro...
An experimental investigation to determine the effects of an accelerating gas flow on the atomizatio...
Statistical regression analysis of Project Pyro cryogenic propellant explosion test dat
Work which has been done at the University of Florida in arriving at credible explosive yield values...
Prediction of yield and other characteristics of liquid propellant rocket explosion
This paper presents a systematic approach by which the expected yield from liquid propellants can be...
The Liquid Propellant Fragment Overpressure Acceleration Model (L-FOAM) is a tool developed by Bangh...
NASA is developing launch vehicles to support missions to Low Earth Orbit (LEO), the moon and deep s...
This paper describes how a mathematical model can be constructed to fit theoretical or experimental ...
During the design phase of large liquid launch vehicles, personnel safety considerations and facilit...
Empirical explosion data from full scale solid rocket launch vehicle accidents and tests were collec...
In order to better understand launch vehicle abort environments, Bangham Engineering Inc. (BEi) buil...
During the design phase of large liquid launch vehicles, personnel safety considerations and facilit...
Flame spreading over surface of igniting solid propellants in different gas mixtures at various pres...
NASA is developing launch vehicles to support missions to Low Earth Orbit (LEO), the moon and deep s...
Data and theory pertinent to the autoignition of liquid oxygen/liquid hydrogen and liquid oxygen pro...
An experimental investigation to determine the effects of an accelerating gas flow on the atomizatio...
Statistical regression analysis of Project Pyro cryogenic propellant explosion test dat
Work which has been done at the University of Florida in arriving at credible explosive yield values...
Prediction of yield and other characteristics of liquid propellant rocket explosion
This paper presents a systematic approach by which the expected yield from liquid propellants can be...
The Liquid Propellant Fragment Overpressure Acceleration Model (L-FOAM) is a tool developed by Bangh...
NASA is developing launch vehicles to support missions to Low Earth Orbit (LEO), the moon and deep s...
This paper describes how a mathematical model can be constructed to fit theoretical or experimental ...
During the design phase of large liquid launch vehicles, personnel safety considerations and facilit...
Empirical explosion data from full scale solid rocket launch vehicle accidents and tests were collec...
In order to better understand launch vehicle abort environments, Bangham Engineering Inc. (BEi) buil...
During the design phase of large liquid launch vehicles, personnel safety considerations and facilit...
Flame spreading over surface of igniting solid propellants in different gas mixtures at various pres...
NASA is developing launch vehicles to support missions to Low Earth Orbit (LEO), the moon and deep s...
Data and theory pertinent to the autoignition of liquid oxygen/liquid hydrogen and liquid oxygen pro...
An experimental investigation to determine the effects of an accelerating gas flow on the atomizatio...