Acoustic data are often required for the determination of launch and powered flight loads for rocket systems and payloads. Such data are usually acquired during test firings of the solid rocket motors. In the current work, these data were obtained for two tests at a remote test facility where we were visitors. This paper describes the data acquisition and the requirements for working at a remote site, interfacing with the test hosts
VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-pr...
The purpose of this work is to develop a method for determining the types of acoustic sources of rad...
A rocket’s turbulent jet radiates intense acoustic waves, which are an acoustic load for structural ...
Acoustic free-field data collected during three reusable solid rocket motor (RSRM) static tests are ...
A new ultrasonic sounding technique to measure the instantaneous propellant thickness in a solid roc...
The payload environment of a rocket is random and dynamic during liftoff and flight, with acoustic n...
As part of an overall program to investigate the vibrational environment of small solid-propellant r...
Energy-based acoustical measurements are investigated in the context of more fully characterizing ro...
Since there is a dearth of flight vibration data and because of the current wide interest in solid-p...
Rocket motors are designed, developed, and evaluated for performance, and after repeated tests, are ...
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
The Space Launch System (SLS) Scale Model Acoustic Test (SMAT) is a 5% scale representation of the S...
The liftoff phase induces acoustic loading over a broad frequency range for a launch vehicle. These ...
This report discusses the purpose and effect of environmental testing, particularly vibration, shock...
College of Engineering; Mechanical & Aerospace Engineering Department; Advisor: Dr. Robert Frederick...
VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-pr...
The purpose of this work is to develop a method for determining the types of acoustic sources of rad...
A rocket’s turbulent jet radiates intense acoustic waves, which are an acoustic load for structural ...
Acoustic free-field data collected during three reusable solid rocket motor (RSRM) static tests are ...
A new ultrasonic sounding technique to measure the instantaneous propellant thickness in a solid roc...
The payload environment of a rocket is random and dynamic during liftoff and flight, with acoustic n...
As part of an overall program to investigate the vibrational environment of small solid-propellant r...
Energy-based acoustical measurements are investigated in the context of more fully characterizing ro...
Since there is a dearth of flight vibration data and because of the current wide interest in solid-p...
Rocket motors are designed, developed, and evaluated for performance, and after repeated tests, are ...
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
The Space Launch System (SLS) Scale Model Acoustic Test (SMAT) is a 5% scale representation of the S...
The liftoff phase induces acoustic loading over a broad frequency range for a launch vehicle. These ...
This report discusses the purpose and effect of environmental testing, particularly vibration, shock...
College of Engineering; Mechanical & Aerospace Engineering Department; Advisor: Dr. Robert Frederick...
VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-pr...
The purpose of this work is to develop a method for determining the types of acoustic sources of rad...
A rocket’s turbulent jet radiates intense acoustic waves, which are an acoustic load for structural ...