Payload Vibration Data Measured During Five Flights Of A Two Stage Solid Propellant Launch Vehicle

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Payload Vibration Data Measured During Five Flights of a Two-stage Solid-propellant Launch Vehicle

Author : Sherman A. Clevenson
Publisher : Unknown
Page : 26 pages
File Size : 42,8 Mb
Release : 1962
Category : Vibration
ISBN : UIUC:30112106915041

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Payload Vibration Data Measured During Five Flights of a Two-stage Solid-propellant Launch Vehicle by Sherman A. Clevenson Pdf

F LIGHT VIBRATION DATA W R OB AINED FROM FIVE VERTICAL ES SHOTS OF Shotput, the lau ch vehicle for v r ical t ts of t e 100-foot infl tabl sp er . T e t o-st ge vehicle consisted of a Pollux an two Recruit rocket motor as the first stage and an ABL X-248 rocket motor as e seco stage. High vibr tion levels w re obtained near bur out of the secon stag of Shotput I, II, and V, hereas only low vibration level were noted on Shotput III and IV. The peak flight vibration levels on Shotput I, II, and V occurred in the longitudinal direction at a frequency of about 570 cps and were about 40g, 45g, and 24g, respectively. The flight vibration levels in t normal and ransverse dir ctions were cons erably le than those in t e longitu inal direction. (Author).

NASA Technical Note

Author : Anonim
Publisher : Unknown
Page : 438 pages
File Size : 47,7 Mb
Release : 1975
Category : Electronic
ISBN : MINN:319510008465504

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NASA Technical Note by Anonim Pdf

U.S. Government Research Reports

Author : Anonim
Publisher : Unknown
Page : 236 pages
File Size : 45,5 Mb
Release : 1962
Category : Science
ISBN : UOM:39015086565820

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U.S. Government Research Reports by Anonim Pdf

Technical Publications Announcements with Indexes

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 1318 pages
File Size : 45,7 Mb
Release : 1962
Category : Aeronautics
ISBN : MINN:31951D00118674L

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Technical Publications Announcements with Indexes by United States. National Aeronautics and Space Administration Pdf

Comparison of Vibrations of a Combination of Solid-rocket Launch Vehicle and Payload During a Ground Firing and Launching

Author : James A. Schoenster
Publisher : Unknown
Page : 44 pages
File Size : 42,8 Mb
Release : 1975
Category : Nike rocket
ISBN : UIUC:30112106916262

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Comparison of Vibrations of a Combination of Solid-rocket Launch Vehicle and Payload During a Ground Firing and Launching by James A. Schoenster Pdf

The results of a study into the environmental vibrations of a payload mounted on the Nike rocket launch vehicle were presented. Data were obtained during the flight acceptance test of the payload, the firing of the total vehicle in a special test stand, and the powered and unpowered flights of the vehicle. The vibrational response of the structure was measured. Data were also obtained on the fluctuating pressure on the outside surface of the vehicle and inside the forward and after ends of the rocket chamber. A comparison of the data from the three test conditions indicated that external pressure fluctuations were the major source of vibrations in the payload area, and pressure fluctuations within the rocket motor were the major source of vibrations contiguous to the payload area.

Applied Mechanics Reviews

Author : Anonim
Publisher : Unknown
Page : 1116 pages
File Size : 45,7 Mb
Release : 1962
Category : Mechanics, Applied
ISBN : UCAL:C2682417

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Applied Mechanics Reviews by Anonim Pdf

Effects of Experimentally Measured Pressure Oscillations on the Vibration of a Solid Rocket Motor

Author : James A. Schoenster,Harold B. Pierce
Publisher : Unknown
Page : 52 pages
File Size : 51,9 Mb
Release : 1972
Category : Nike rocket
ISBN : UIUC:30112106641019

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Effects of Experimentally Measured Pressure Oscillations on the Vibration of a Solid Rocket Motor by James A. Schoenster,Harold B. Pierce Pdf

Results are presented of firing a Nike rocket against a backstop for the purpose of obtaining pressure fluctuations in the rocket case and determining their relationship to structural vibrations of the case. Special care was required to obtain these pressure fluctuations because of the much higher static pressure generated in the rocket. Very small pressure fluctuations within the rocket case can cause significant vibration levels. A previously observed high frequency was shown to decrease with time before completely disappearing at about 1 second of burning time. The vibration of the case itself is probably related to the longitudinal structural modes at frequencies below 500 Hz and is dependent on local structural conditions at frequencies above this value.

Publications of Goddard Space Flight Center

Author : Goddard Space Flight Center
Publisher : Unknown
Page : 804 pages
File Size : 52,8 Mb
Release : 1959
Category : Astronautics
ISBN : PSU:000003511572

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Publications of Goddard Space Flight Center by Goddard Space Flight Center Pdf

Astronautics Information Abstracts

Author : Anonim
Publisher : Unknown
Page : 60 pages
File Size : 45,5 Mb
Release : 1962
Category : Astronautics
ISBN : UVA:X004946828

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Astronautics Information Abstracts by Anonim Pdf

Astronautics Information

Author : Jet Propulsion Laboratory (U.S.).
Publisher : Unknown
Page : 288 pages
File Size : 50,6 Mb
Release : 1962
Category : Astronautics
ISBN : STANFORD:36105027884134

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Astronautics Information by Jet Propulsion Laboratory (U.S.). Pdf

Environmental Effects on Materials and Equipment

Author : Anonim
Publisher : Unknown
Page : 860 pages
File Size : 52,7 Mb
Release : 1962
Category : Environmental engineering
ISBN : UOM:39015020154962

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Environmental Effects on Materials and Equipment by Anonim Pdf

Beginning in 1962 issued in sections A and B.

Journal of the Royal Aeronautical Society

Author : Royal Aeronautical Society
Publisher : Unknown
Page : 1164 pages
File Size : 46,6 Mb
Release : 1962
Category : Aeronautics
ISBN : MINN:319510006533321

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Journal of the Royal Aeronautical Society by Royal Aeronautical Society Pdf