Welcome
to Vibrationdata
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Astronaut Michael Collins wrote:The first stage of the Titan II vibrated longitudinally, so that someone riding on it would be bounced up and down as if on a pogo stick. The vibration was at a relatively high frequency, about 11 cycles per second, with an amplitude of plus or minus 5 Gs in the worst case.
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VIBROACOUSTICS
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BARRETT METHODSNASA
TN D-1836, Techniques for Predicting Localized Vibratory Environments
of Rocket Vehicles: NASA_TN_D1836.pdf NASA TN D-2158, Statistical Techniques for Predicting Localized Vibratory Environments of Rocket Vehicles: Barrett-TN-D-2158-1964.pdf |
LIFTOFF ACOUSTICS NASA SP-8072, Acoustic Loads Generated by the Propulsion System: sp8072.pdfHaynes & Kenny, Modifications to the NASA SP-8072 Distributed Source Method II for Ares I Lift-off Environment Predictions: NASA_SP8072_Ares_I.pdf ATK Launch Vehicle (ALV-X1) Liftoff Acoustic Environments: Prediction vs. Measurement ALV_X1_liftoff_acoustics.pdf Peter Franken, Methods of Space Vehicle Noise Prediction, WADC Technical Report 58-343, Volume II: Franken_acoustics.pdf Launch Vehicle Liftoff Acoustics Scaled from Ground to Air-Launch: aco_ground_air_launch.pdf Rocket Vehicle Liftoff Acoustics, Part I: Acoustic Pressure near Nozzle Exit Plane: liftoff.pdf Rocket Vehicle Liftoff Acoustics, Part III: Acoustic Attenuation: lift_att.pdf |
EFFECT OF A ROCKET LAUNCH ENVIRONMENT ON GROUND EQUIPMENTSonic and Vibration Environments for Ground Facilities - A Design Manual, Prepared for NASA by Wyle Laboratories: sonic_ground.pdfAtmospheric Sound Propagation from a Monopole Source via Direct, Reflected, and Surface Waves: direct_reflected.pdfAtmospheric Absorption: atmospheric_absorption.pdfMatlab ScriptsAdjustment of SPL for ambient temperature and pressure: SPL_change_ambient.mAtmospheric Absorption: atmosphere_absorption.mSpherical propagation
from a point source through the atmosphere with both direct and ground
reflected waves:
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CASSININASA/TM-2000-209387, Investigation of Acoustic Fields for the Cassini Spacecraft: Reverberant Versus Launch Environment: Cassini_acoustics.pdfCassini Spacecraft Acoustic Flight and Test Criteria: Cassini_acoustic_criteria.pdf |
PAYLOAD ACOUSTICS - Acoustic Blankets, Melamine Foam Moved to: Vibroacoustics Page |
PAYLOAD ACOUSTICS - Fill Factors, Testing, etc.Moved to: Vibroacoustics Page |
SOLID MOTOR PRESSURE OSCILLATIONSSolid Rocket
Motor Pressure Oscillation Frequencies: solid_motor_oscillation.pdf
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LIQUID ENGINE
POGO & PRESSURE OSCILLATIONS
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MAIN ENGINE CUT-OFF (MECO)Scott Gordon, Delta II
MECO Transient: A Payload Perspective: MECO_trans_elv2002.pdf
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PEGASUSThe Pegasus Launch
Vehicle: Shock and Vibration Environments PegasusSV.pdf
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PROPELLANT SLOSH
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FLUTTER
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ARES & ARES 1-XDr. Steve Ryan, Vibration Challenges in the Design of NASA's Ares Launch Vehicles: Ares_vibration_challenges.pdfDan Niedermaier & Mo Kaouk, Ares 1X Hybrid Modeling with Comparisons to Flight Data: 36_Dan Niedermaier.pdfAres 1-X Flight Data, APO-1041: Ares_1X_flight_data.pdf |
COMBINED LOADS Combined
Ascent Loads for Launch Vehicle Analysis: Combined_loads.pdf NASA, Combination Methods for Deriving Structural Design Loads Considering Vibro-Acoustic, etc., Responses: combining_VA.pdf |
SPACECRAFT & PAYLOAD STRUCTURAL DYNAMICSSample Lateral Natural
Frequency Calculations for a Space Vehicle/Dispenser Analysis: lateralSV.pdf
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FUEL INJECTORS & CAVITATING VENTURIT. Irvine, Cavitating Venturi Oscillation: cavitating_venturi.pdf Miller, Anderson, Heister; Investigation of Liquid Rocket Injector Element Stability Margins: Anderson_cv.pdfSchmidt, Su, Goney, Farrell, Corradini; Detection of Cavitation in Fuel Injector Nozzles: Schmidt_cv.pdf |
OTHER TUTORIALSChristensen,
Brown, Frady, Calculation of Dynamic Load Due to Random Vibration
Environments in Rocket Engine Systems: Rocket_Engines_Dynamic_Loads.pdf
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Software |
Executable |
Source |
Liftoff Acoustics of Rocket Vehicle. |
liftoff.exe |
liftoff.cppsp8072.pdfRocket_Motor_Values.pdfliftoff_notes.pdf |
Liftoff Undeflected, Hybrid Methods 1 & 2 |
liftoff_h_undeflected.exe |
liftoff_h_undeflected.cpp |
Liftoff, Hybrid Methods 1 & 2 |
liftoff_hyrbrid.exe |
liftoff_hybrid.cpp |
Acoustic Pressure Field surrounding Rocket Vehicle during Ascent. |
flow.exe |
flow.cpp |
flowtable.exe |
flowtable.cpp |
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Ring frequency for a cylindrical structure. |
Windows:
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ring_mode.cpp |
Franken method for a cylindrical structure subjected to a sound pressure field. |
Franken.exe |
Franken.cpp |
Mass Loading Attenuation Factor for Heavy Equipment and Payloads |
mass_attenuation.exe |
mass_attenuation.cpp |
Newsletters with Rocket and Spacecraft Articles
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Book Recommendations
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