Free Flight Range Tests of a High Density Armor Piercing Flechette Utilizing Yaw cards

Aerodynamic stability and drag data were obtained from yaw card tests of the high density armor piercing flechette. The test items encased in aluminum sabots, were launched from a 30mm smooth bore powder gun. The sabot petals were deflected by a steel cone, 22 feet from the muzzle smooth bore powder...

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Winchenbach, G. L
description Aerodynamic stability and drag data were obtained from yaw card tests of the high density armor piercing flechette. The test items encased in aluminum sabots, were launched from a 30mm smooth bore powder gun. The sabot petals were deflected by a steel cone, 22 feet from the muzzle smooth bore powder gun. The test item then proceeded through the instrumented portion of the range, passing through 20 yaw cards spaced approximately 10 feet apart. Six velocity measurements were obtained when the projectile punched holes in 12 sheets of circuit paper; one sheet started a chronograph and the second sheet stopped the chronograph. Aerodynamic stability data were obtained by analyzing successive holes cut in the yaw cards by the projectile. The drag data were derived from the measured reduction in velocity as the projectile traversed the range. The tests were conducted over a Mach number range of 1.25 to 2.25.
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L ; AIR FORCE ARMAMENT LAB EGLIN AFB FL</creatorcontrib><description>Aerodynamic stability and drag data were obtained from yaw card tests of the high density armor piercing flechette. The test items encased in aluminum sabots, were launched from a 30mm smooth bore powder gun. The sabot petals were deflected by a steel cone, 22 feet from the muzzle smooth bore powder gun. The test item then proceeded through the instrumented portion of the range, passing through 20 yaw cards spaced approximately 10 feet apart. Six velocity measurements were obtained when the projectile punched holes in 12 sheets of circuit paper; one sheet started a chronograph and the second sheet stopped the chronograph. Aerodynamic stability data were obtained by analyzing successive holes cut in the yaw cards by the projectile. The drag data were derived from the measured reduction in velocity as the projectile traversed the range. The tests were conducted over a Mach number range of 1.25 to 2.25.</description><language>eng</language><subject>30-mm guns ; AERODYNAMIC DRAG ; AERODYNAMIC STABILITY ; ALUMINUM ; Ammunition and Explosives ; ANTITANK WEAPONS ; ARMOR PIERCING AMMUNITION ; Ballistics ; CARDS ; CHRONOMETERS ; DATA REDUCTION ; Discarding sabot projectiles ; EXTERIOR BALLISTICS ; FIN STABILIZED AMMUNITION ; FIRING TESTS(ORDNANCE) ; FLECHETTES ; Fluid Mechanics ; FREE FLIGHT MODELS ; FREE FLIGHT TRAJECTORIES ; GUN LAUNCHERS ; HDAP(High density armor piercing) ; HIGH DENSITY ; High density armor piercing projectiles ; LOW COSTS ; SABOT PROJECTILES ; SABOTS ; SEPARATION ; SPINNING(MOTION) ; STATIC STABILITY ; SUPERSONIC CHARACTERISTICS ; TEST EQUIPMENT ; Witness cards ; YAW ; Yaw cards</subject><creationdate>1974</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27545,27546</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0919937$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Mayer, Paul C</creatorcontrib><creatorcontrib>Winchenbach, G. 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The drag data were derived from the measured reduction in velocity as the projectile traversed the range. The tests were conducted over a Mach number range of 1.25 to 2.25.</description><subject>30-mm guns</subject><subject>AERODYNAMIC DRAG</subject><subject>AERODYNAMIC STABILITY</subject><subject>ALUMINUM</subject><subject>Ammunition and Explosives</subject><subject>ANTITANK WEAPONS</subject><subject>ARMOR PIERCING AMMUNITION</subject><subject>Ballistics</subject><subject>CARDS</subject><subject>CHRONOMETERS</subject><subject>DATA REDUCTION</subject><subject>Discarding sabot projectiles</subject><subject>EXTERIOR BALLISTICS</subject><subject>FIN STABILIZED AMMUNITION</subject><subject>FIRING TESTS(ORDNANCE)</subject><subject>FLECHETTES</subject><subject>Fluid Mechanics</subject><subject>FREE FLIGHT MODELS</subject><subject>FREE FLIGHT TRAJECTORIES</subject><subject>GUN LAUNCHERS</subject><subject>HDAP(High density armor piercing)</subject><subject>HIGH DENSITY</subject><subject>High density armor piercing projectiles</subject><subject>LOW COSTS</subject><subject>SABOT PROJECTILES</subject><subject>SABOTS</subject><subject>SEPARATION</subject><subject>SPINNING(MOTION)</subject><subject>STATIC STABILITY</subject><subject>SUPERSONIC CHARACTERISTICS</subject><subject>TEST EQUIPMENT</subject><subject>Witness cards</subject><subject>YAW</subject><subject>Yaw cards</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1974</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFi7EKwjAQQLM4iPoHDvcDgtJBMpbW0FGkCk7lSK_pQUwhdyD69VZwd3rwHm9pbi4TgYscRoULpkDQkqjANABCM2uoKQnrC8r8mDKcmbLnFOaH_EiqBFflyO-vu-MTPOZe1mYxYBTa_LgyW3dqq2bXK_tOlBNpV9Z7e7C2OBZ_8gcWgzU8</recordid><startdate>197404</startdate><enddate>197404</enddate><creator>Mayer, Paul C</creator><creator>Winchenbach, G. 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The test item then proceeded through the instrumented portion of the range, passing through 20 yaw cards spaced approximately 10 feet apart. Six velocity measurements were obtained when the projectile punched holes in 12 sheets of circuit paper; one sheet started a chronograph and the second sheet stopped the chronograph. Aerodynamic stability data were obtained by analyzing successive holes cut in the yaw cards by the projectile. The drag data were derived from the measured reduction in velocity as the projectile traversed the range. The tests were conducted over a Mach number range of 1.25 to 2.25.</abstract><oa>free_for_read</oa></addata></record>
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source DTIC Technical Reports
subjects 30-mm guns
AERODYNAMIC DRAG
AERODYNAMIC STABILITY
ALUMINUM
Ammunition and Explosives
ANTITANK WEAPONS
ARMOR PIERCING AMMUNITION
Ballistics
CARDS
CHRONOMETERS
DATA REDUCTION
Discarding sabot projectiles
EXTERIOR BALLISTICS
FIN STABILIZED AMMUNITION
FIRING TESTS(ORDNANCE)
FLECHETTES
Fluid Mechanics
FREE FLIGHT MODELS
FREE FLIGHT TRAJECTORIES
GUN LAUNCHERS
HDAP(High density armor piercing)
HIGH DENSITY
High density armor piercing projectiles
LOW COSTS
SABOT PROJECTILES
SABOTS
SEPARATION
SPINNING(MOTION)
STATIC STABILITY
SUPERSONIC CHARACTERISTICS
TEST EQUIPMENT
Witness cards
YAW
Yaw cards
title Free Flight Range Tests of a High Density Armor Piercing Flechette Utilizing Yaw cards
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