Loading…

SHOCK AND VIBRATION BULLETIN NO. 20

Contents: Designing for shock. A status rept The compatibility of shock spectra with shock design factors Measurements of rocket thrust at frequencies up to 4000 cps Controlling shock and vibration by friction damping Type approval of guided missile container shock isolators Displacement needed in s...

Full description

Saved in:
Bibliographic Details
Main Author: OFFICE OF THE SECRETARY OF DEFENSE (RESEARCH AND ENGINEERING) WASHINGTON DC
Format: Report
Language:English
Subjects:
Online Access:Request full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by
cites
container_end_page
container_issue
container_start_page
container_title
container_volume
creator OFFICE OF THE SECRETARY OF DEFENSE (RESEARCH AND ENGINEERING) WASHINGTON DC
description Contents: Designing for shock. A status rept The compatibility of shock spectra with shock design factors Measurements of rocket thrust at frequencies up to 4000 cps Controlling shock and vibration by friction damping Type approval of guided missile container shock isolators Displacement needed in shock isolation Evaluating shock and vibration resistance in terms of laboratory test failures Forces acting on a shipping container in transit Missile reliability in jeopardy Some factors in the design of package cushioning Concepts and needs in the over-all problem for shipping missiles Simulating mile-long rapidly applied acceleration in the laboratory Theory and design of aerial camera vibration isolation and stabilization A portable 100-ft drop tester Proposed tests for escape from very high velocity aircraft Flight vibration characteristics of F-86-A5 airplane with machine guns firing Design of clock-type mechanisms to meet extreme shock and vibration requirements The development and use of a statistical accelerometer Concepts of specifications in mobile military gear Design objectives for package shock recording instrumentation Use of the energy method in the design of package cushions Shock tests against the USS ULUA (SS428) Validity of accelerated vibration testing by increasing amplitude and decreasing time of test (Not abstracted. See also AD 9513)
format report
fullrecord <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_AD0020061</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>AD0020061</sourcerecordid><originalsourceid>FETCH-dtic_stinet_AD00200613</originalsourceid><addsrcrecordid>eNrjZFAO9vB39lZw9HNRCPN0CnIM8fT3U3AK9fFxDfH0U_Dz11MwMuBhYE1LzClO5YXS3Awybq4hzh66KSWZyfHFJZl5qSXxji4GBkYGBmaGxgSkAdIbHxs</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>SHOCK AND VIBRATION BULLETIN NO. 20</title><source>DTIC Technical Reports</source><creator>OFFICE OF THE SECRETARY OF DEFENSE (RESEARCH AND ENGINEERING) WASHINGTON DC</creator><creatorcontrib>OFFICE OF THE SECRETARY OF DEFENSE (RESEARCH AND ENGINEERING) WASHINGTON DC</creatorcontrib><description>Contents: Designing for shock. A status rept The compatibility of shock spectra with shock design factors Measurements of rocket thrust at frequencies up to 4000 cps Controlling shock and vibration by friction damping Type approval of guided missile container shock isolators Displacement needed in shock isolation Evaluating shock and vibration resistance in terms of laboratory test failures Forces acting on a shipping container in transit Missile reliability in jeopardy Some factors in the design of package cushioning Concepts and needs in the over-all problem for shipping missiles Simulating mile-long rapidly applied acceleration in the laboratory Theory and design of aerial camera vibration isolation and stabilization A portable 100-ft drop tester Proposed tests for escape from very high velocity aircraft Flight vibration characteristics of F-86-A5 airplane with machine guns firing Design of clock-type mechanisms to meet extreme shock and vibration requirements The development and use of a statistical accelerometer Concepts of specifications in mobile military gear Design objectives for package shock recording instrumentation Use of the energy method in the design of package cushions Shock tests against the USS ULUA (SS428) Validity of accelerated vibration testing by increasing amplitude and decreasing time of test (Not abstracted. See also AD 9513)</description><language>eng</language><subject>ACCELERATED TESTING ; ACCELERATION ; ACCELEROMETERS ; AERIAL CAMERAS ; COMPATIBILITY ; CUSHIONING ; DAMPING ; ENERGY ; FRICTION ; GEARS ; Guided Missile Launching and Basing Support ; GUIDED MISSILES ; ISOLATION ; LABORATORIES ; MACHINE GUNS ; MEASUREMENT ; MOBILE ; RELIABILITY ; REQUIREMENTS ; RESISTANCE ; Rocket Engines ; ROCKETS ; SHIPPING ; SHIPPING CONTAINERS ; SHOCK ; SHOCK SPECTRA ; SHOCK TESTS ; STATISTICS ; TEST AND EVALUATION ; Test Facilities, Equipment and Methods ; THEORY ; THRUST ; TIME ; VIBRATION ; VIBRATION ISOLATORS</subject><creationdate>1953</creationdate><rights>Approved for public release; distribution is unlimited. Document partially illegible.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0020061$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>OFFICE OF THE SECRETARY OF DEFENSE (RESEARCH AND ENGINEERING) WASHINGTON DC</creatorcontrib><title>SHOCK AND VIBRATION BULLETIN NO. 20</title><description>Contents: Designing for shock. A status rept The compatibility of shock spectra with shock design factors Measurements of rocket thrust at frequencies up to 4000 cps Controlling shock and vibration by friction damping Type approval of guided missile container shock isolators Displacement needed in shock isolation Evaluating shock and vibration resistance in terms of laboratory test failures Forces acting on a shipping container in transit Missile reliability in jeopardy Some factors in the design of package cushioning Concepts and needs in the over-all problem for shipping missiles Simulating mile-long rapidly applied acceleration in the laboratory Theory and design of aerial camera vibration isolation and stabilization A portable 100-ft drop tester Proposed tests for escape from very high velocity aircraft Flight vibration characteristics of F-86-A5 airplane with machine guns firing Design of clock-type mechanisms to meet extreme shock and vibration requirements The development and use of a statistical accelerometer Concepts of specifications in mobile military gear Design objectives for package shock recording instrumentation Use of the energy method in the design of package cushions Shock tests against the USS ULUA (SS428) Validity of accelerated vibration testing by increasing amplitude and decreasing time of test (Not abstracted. See also AD 9513)</description><subject>ACCELERATED TESTING</subject><subject>ACCELERATION</subject><subject>ACCELEROMETERS</subject><subject>AERIAL CAMERAS</subject><subject>COMPATIBILITY</subject><subject>CUSHIONING</subject><subject>DAMPING</subject><subject>ENERGY</subject><subject>FRICTION</subject><subject>GEARS</subject><subject>Guided Missile Launching and Basing Support</subject><subject>GUIDED MISSILES</subject><subject>ISOLATION</subject><subject>LABORATORIES</subject><subject>MACHINE GUNS</subject><subject>MEASUREMENT</subject><subject>MOBILE</subject><subject>RELIABILITY</subject><subject>REQUIREMENTS</subject><subject>RESISTANCE</subject><subject>Rocket Engines</subject><subject>ROCKETS</subject><subject>SHIPPING</subject><subject>SHIPPING CONTAINERS</subject><subject>SHOCK</subject><subject>SHOCK SPECTRA</subject><subject>SHOCK TESTS</subject><subject>STATISTICS</subject><subject>TEST AND EVALUATION</subject><subject>Test Facilities, Equipment and Methods</subject><subject>THEORY</subject><subject>THRUST</subject><subject>TIME</subject><subject>VIBRATION</subject><subject>VIBRATION ISOLATORS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1953</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZFAO9vB39lZw9HNRCPN0CnIM8fT3U3AK9fFxDfH0U_Dz11MwMuBhYE1LzClO5YXS3Awybq4hzh66KSWZyfHFJZl5qSXxji4GBkYGBmaGxgSkAdIbHxs</recordid><startdate>195305</startdate><enddate>195305</enddate><creator>OFFICE OF THE SECRETARY OF DEFENSE (RESEARCH AND ENGINEERING) WASHINGTON DC</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>195305</creationdate><title>SHOCK AND VIBRATION BULLETIN NO. 20</title></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD00200613</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1953</creationdate><topic>ACCELERATED TESTING</topic><topic>ACCELERATION</topic><topic>ACCELEROMETERS</topic><topic>AERIAL CAMERAS</topic><topic>COMPATIBILITY</topic><topic>CUSHIONING</topic><topic>DAMPING</topic><topic>ENERGY</topic><topic>FRICTION</topic><topic>GEARS</topic><topic>Guided Missile Launching and Basing Support</topic><topic>GUIDED MISSILES</topic><topic>ISOLATION</topic><topic>LABORATORIES</topic><topic>MACHINE GUNS</topic><topic>MEASUREMENT</topic><topic>MOBILE</topic><topic>RELIABILITY</topic><topic>REQUIREMENTS</topic><topic>RESISTANCE</topic><topic>Rocket Engines</topic><topic>ROCKETS</topic><topic>SHIPPING</topic><topic>SHIPPING CONTAINERS</topic><topic>SHOCK</topic><topic>SHOCK SPECTRA</topic><topic>SHOCK TESTS</topic><topic>STATISTICS</topic><topic>TEST AND EVALUATION</topic><topic>Test Facilities, Equipment and Methods</topic><topic>THEORY</topic><topic>THRUST</topic><topic>TIME</topic><topic>VIBRATION</topic><topic>VIBRATION ISOLATORS</topic><toplevel>online_resources</toplevel><creatorcontrib>OFFICE OF THE SECRETARY OF DEFENSE (RESEARCH AND ENGINEERING) WASHINGTON DC</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><aucorp>OFFICE OF THE SECRETARY OF DEFENSE (RESEARCH AND ENGINEERING) WASHINGTON DC</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>SHOCK AND VIBRATION BULLETIN NO. 20</btitle><date>1953-05</date><risdate>1953</risdate><abstract>Contents: Designing for shock. A status rept The compatibility of shock spectra with shock design factors Measurements of rocket thrust at frequencies up to 4000 cps Controlling shock and vibration by friction damping Type approval of guided missile container shock isolators Displacement needed in shock isolation Evaluating shock and vibration resistance in terms of laboratory test failures Forces acting on a shipping container in transit Missile reliability in jeopardy Some factors in the design of package cushioning Concepts and needs in the over-all problem for shipping missiles Simulating mile-long rapidly applied acceleration in the laboratory Theory and design of aerial camera vibration isolation and stabilization A portable 100-ft drop tester Proposed tests for escape from very high velocity aircraft Flight vibration characteristics of F-86-A5 airplane with machine guns firing Design of clock-type mechanisms to meet extreme shock and vibration requirements The development and use of a statistical accelerometer Concepts of specifications in mobile military gear Design objectives for package shock recording instrumentation Use of the energy method in the design of package cushions Shock tests against the USS ULUA (SS428) Validity of accelerated vibration testing by increasing amplitude and decreasing time of test (Not abstracted. See also AD 9513)</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_dtic_stinet_AD0020061
source DTIC Technical Reports
subjects ACCELERATED TESTING
ACCELERATION
ACCELEROMETERS
AERIAL CAMERAS
COMPATIBILITY
CUSHIONING
DAMPING
ENERGY
FRICTION
GEARS
Guided Missile Launching and Basing Support
GUIDED MISSILES
ISOLATION
LABORATORIES
MACHINE GUNS
MEASUREMENT
MOBILE
RELIABILITY
REQUIREMENTS
RESISTANCE
Rocket Engines
ROCKETS
SHIPPING
SHIPPING CONTAINERS
SHOCK
SHOCK SPECTRA
SHOCK TESTS
STATISTICS
TEST AND EVALUATION
Test Facilities, Equipment and Methods
THEORY
THRUST
TIME
VIBRATION
VIBRATION ISOLATORS
title SHOCK AND VIBRATION BULLETIN NO. 20
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-23T23%3A37%3A59IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-dtic_1RU&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=SHOCK%20AND%20VIBRATION%20BULLETIN%20NO.%2020&rft.aucorp=OFFICE%20OF%20THE%20SECRETARY%20OF%20DEFENSE%20(RESEARCH%20AND%20ENGINEERING)%20WASHINGTON%20DC&rft.date=1953-05&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EAD0020061%3C/dtic_1RU%3E%3Cgrp_id%3Ecdi_FETCH-dtic_stinet_AD00200613%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true