Fluidic Generator to Power Rocket Proximity Fuze
A fluidic generator has been designed to satisfy the power requirement of a rocket proximity fuze. The design was based on the generator used with the XM445 time fuze for the Multiple Launch Rocket System (MLRS). Power output was increased to approximately 5 W at pressure above 10 psig by increasing...
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| creator | Campagnuolo, Carl J |
| description | A fluidic generator has been designed to satisfy the power requirement of a rocket proximity fuze. The design was based on the generator used with the XM445 time fuze for the Multiple Launch Rocket System (MLRS). Power output was increased to approximately 5 W at pressure above 10 psig by increasing the diameter of the coil wire (No. 30 versus 36 AWG), reducing the number of turns (559 versus 1500), and increasing the value of the coupling capacitor (0.4 versus 0.022 micrometer F) to achieve optimum matching into a 120 load. The product was evaluated in a configuration where open space within the fuze nose cone was reduced to accommodate a fuze antenna. The ability of the generator to survive pressure extremes normally encountered by MLRS flight and to provide sustaining power to a complementary metal-oxide-semiconductor timer at flight apogee was successfully demonstrated. The fluidic generator retains its ability to provide a second independent environmental signature to the safety and arming device. |
| format | Report |
| fullrecord | <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_ADA131062</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ADA131062</sourcerecordid><originalsourceid>FETCH-dtic_stinet_ADA1310623</originalsourceid><addsrcrecordid>eNrjZDBwyynNTMlMVnBPzUstSizJL1IoyVcIyC9PLVIIyk_OTi1RCCjKr8jMzSypVHArrUrlYWBNS8wpTuWF0twMMm6uIc4euiklmcnxxSWZeakl8Y4ujobGhgZmRsYEpAGVACgb</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Fluidic Generator to Power Rocket Proximity Fuze</title><source>DTIC Technical Reports</source><creator>Campagnuolo, Carl J</creator><creatorcontrib>Campagnuolo, Carl J ; HARRY DIAMOND LABS ADELPHI MD</creatorcontrib><description>A fluidic generator has been designed to satisfy the power requirement of a rocket proximity fuze. The design was based on the generator used with the XM445 time fuze for the Multiple Launch Rocket System (MLRS). Power output was increased to approximately 5 W at pressure above 10 psig by increasing the diameter of the coil wire (No. 30 versus 36 AWG), reducing the number of turns (559 versus 1500), and increasing the value of the coupling capacitor (0.4 versus 0.022 micrometer F) to achieve optimum matching into a 120 load. The product was evaluated in a configuration where open space within the fuze nose cone was reduced to accommodate a fuze antenna. The ability of the generator to survive pressure extremes normally encountered by MLRS flight and to provide sustaining power to a complementary metal-oxide-semiconductor timer at flight apogee was successfully demonstrated. The fluidic generator retains its ability to provide a second independent environmental signature to the safety and arming device.</description><language>eng</language><subject>Ammunition and Explosives ; ARMING DEVICES ; ASE76 ; CONFIGURATIONS ; Electric Power Production and Distribution ; ENVIRONMENTS ; EXPERIMENTAL DESIGN ; FLUIDIC GENERATORS ; FLUIDICS ; Fluidics and Fluerics ; GENERATORS ; LPN-HDL-461246 ; LPN-PRON-1A2D5A26011AA9 ; MLRS(MULTIPLE LAUNCH ROCKET SYSTEM) ; PE63615D ; PERMANENT MAGNETS ; POWER SUPPLIES ; PROXIMITY FUZES ; ROCKET LAUNCHING ; SAFETY ; TEST AND EVALUATION</subject><creationdate>1983</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA131062$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Campagnuolo, Carl J</creatorcontrib><creatorcontrib>HARRY DIAMOND LABS ADELPHI MD</creatorcontrib><title>Fluidic Generator to Power Rocket Proximity Fuze</title><description>A fluidic generator has been designed to satisfy the power requirement of a rocket proximity fuze. The design was based on the generator used with the XM445 time fuze for the Multiple Launch Rocket System (MLRS). Power output was increased to approximately 5 W at pressure above 10 psig by increasing the diameter of the coil wire (No. 30 versus 36 AWG), reducing the number of turns (559 versus 1500), and increasing the value of the coupling capacitor (0.4 versus 0.022 micrometer F) to achieve optimum matching into a 120 load. The product was evaluated in a configuration where open space within the fuze nose cone was reduced to accommodate a fuze antenna. The ability of the generator to survive pressure extremes normally encountered by MLRS flight and to provide sustaining power to a complementary metal-oxide-semiconductor timer at flight apogee was successfully demonstrated. The fluidic generator retains its ability to provide a second independent environmental signature to the safety and arming device.</description><subject>Ammunition and Explosives</subject><subject>ARMING DEVICES</subject><subject>ASE76</subject><subject>CONFIGURATIONS</subject><subject>Electric Power Production and Distribution</subject><subject>ENVIRONMENTS</subject><subject>EXPERIMENTAL DESIGN</subject><subject>FLUIDIC GENERATORS</subject><subject>FLUIDICS</subject><subject>Fluidics and Fluerics</subject><subject>GENERATORS</subject><subject>LPN-HDL-461246</subject><subject>LPN-PRON-1A2D5A26011AA9</subject><subject>MLRS(MULTIPLE LAUNCH ROCKET SYSTEM)</subject><subject>PE63615D</subject><subject>PERMANENT MAGNETS</subject><subject>POWER SUPPLIES</subject><subject>PROXIMITY FUZES</subject><subject>ROCKET LAUNCHING</subject><subject>SAFETY</subject><subject>TEST AND EVALUATION</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1983</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZDBwyynNTMlMVnBPzUstSizJL1IoyVcIyC9PLVIIyk_OTi1RCCjKr8jMzSypVHArrUrlYWBNS8wpTuWF0twMMm6uIc4euiklmcnxxSWZeakl8Y4ujobGhgZmRsYEpAGVACgb</recordid><startdate>198307</startdate><enddate>198307</enddate><creator>Campagnuolo, Carl J</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>198307</creationdate><title>Fluidic Generator to Power Rocket Proximity Fuze</title><author>Campagnuolo, Carl J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA1310623</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1983</creationdate><topic>Ammunition and Explosives</topic><topic>ARMING DEVICES</topic><topic>ASE76</topic><topic>CONFIGURATIONS</topic><topic>Electric Power Production and Distribution</topic><topic>ENVIRONMENTS</topic><topic>EXPERIMENTAL DESIGN</topic><topic>FLUIDIC GENERATORS</topic><topic>FLUIDICS</topic><topic>Fluidics and Fluerics</topic><topic>GENERATORS</topic><topic>LPN-HDL-461246</topic><topic>LPN-PRON-1A2D5A26011AA9</topic><topic>MLRS(MULTIPLE LAUNCH ROCKET SYSTEM)</topic><topic>PE63615D</topic><topic>PERMANENT MAGNETS</topic><topic>POWER SUPPLIES</topic><topic>PROXIMITY FUZES</topic><topic>ROCKET LAUNCHING</topic><topic>SAFETY</topic><topic>TEST AND EVALUATION</topic><toplevel>online_resources</toplevel><creatorcontrib>Campagnuolo, Carl J</creatorcontrib><creatorcontrib>HARRY DIAMOND LABS ADELPHI MD</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Campagnuolo, Carl J</au><aucorp>HARRY DIAMOND LABS ADELPHI MD</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Fluidic Generator to Power Rocket Proximity Fuze</btitle><date>1983-07</date><risdate>1983</risdate><abstract>A fluidic generator has been designed to satisfy the power requirement of a rocket proximity fuze. The design was based on the generator used with the XM445 time fuze for the Multiple Launch Rocket System (MLRS). Power output was increased to approximately 5 W at pressure above 10 psig by increasing the diameter of the coil wire (No. 30 versus 36 AWG), reducing the number of turns (559 versus 1500), and increasing the value of the coupling capacitor (0.4 versus 0.022 micrometer F) to achieve optimum matching into a 120 load. The product was evaluated in a configuration where open space within the fuze nose cone was reduced to accommodate a fuze antenna. The ability of the generator to survive pressure extremes normally encountered by MLRS flight and to provide sustaining power to a complementary metal-oxide-semiconductor timer at flight apogee was successfully demonstrated. The fluidic generator retains its ability to provide a second independent environmental signature to the safety and arming device.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
| recordid | cdi_dtic_stinet_ADA131062 |
| source | DTIC Technical Reports |
| subjects | Ammunition and Explosives ARMING DEVICES ASE76 CONFIGURATIONS Electric Power Production and Distribution ENVIRONMENTS EXPERIMENTAL DESIGN FLUIDIC GENERATORS FLUIDICS Fluidics and Fluerics GENERATORS LPN-HDL-461246 LPN-PRON-1A2D5A26011AA9 MLRS(MULTIPLE LAUNCH ROCKET SYSTEM) PE63615D PERMANENT MAGNETS POWER SUPPLIES PROXIMITY FUZES ROCKET LAUNCHING SAFETY TEST AND EVALUATION |
| title | Fluidic Generator to Power Rocket Proximity Fuze |
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