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Development of a high-velocity free-flight launcher : the Ames light-gas gunRecent interest in long-range missiles has stimulated a search for new experimental techniques which can reproduce in the laboratory the high temperatures and Mach numbers associated with the missiles' flight. One promising possibility lies in free-flight testing of laboratory models which are flown at the full velocity of the missile. In this type of test, temperatures are approximated and aerodynamic heating of the model is representative of that experienced by the missile in high-velocity flight. A prime requirement of the free-flight test technique is a device which had the capacity for launching models at the velocities desired. In response to thie need, a gun firing light models at velocities up to 15,000 feet per second has been developed at the Ames Aeronautical Laboratory. The design of this gun, the analysis of its performance, and the results of the initial firing trials are described in this paper. The firing trials showed that the measured velocities and pressures agreed well with the predicted values. Also, the erosion of the launch tube was very small for the eleven rounds fired. The performance of the gun suggests that it will prove to be a satisfactory launcher for high-velocity free-flight tests. However, it should be mentioned that only the gross performance has been evaluated so far, and, consequently, the operation of the gun must be investigated in further detail before its performance can be reliably predicted over its full operating range.
Document ID
19930093745
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Charters, A C
Denardo, B Pat
Rossow, Vernon J
Date Acquired
August 29, 2013
Publication Date
December 28, 1955
Report/Patent Number
NACA-RM-A55G11
Report Number: NACA-RM-A55G11
Accession Number
93R23046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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