Thermally Stable Burning Rate Accelerators
The purpose of this program is to research the methods and materials that will produce thermally stable AP and burning rate catalyst. They will be used with other thermally stable propellant ingredients to produce a solid propellant that is capable of withstanding a temperature environment of -75 to...
Gespeichert in:
| Hauptverfasser: | , , , , |
|---|---|
| Format: | Report |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | Stephens, W D Flanigan, D A Hightower, J O Miller, M Willis, T C |
| description | The purpose of this program is to research the methods and materials that will produce thermally stable AP and burning rate catalyst. They will be used with other thermally stable propellant ingredients to produce a solid propellant that is capable of withstanding a temperature environment of -75 to 350 F. With the present capability of aircraft to fly at supersonic speeds, a new requirement now exists for missiles which can be carried externally. The major development problem arises from the effects of aerodynamic heating, causing missile skin temperatures of several hundred degrees Fahrenheit. In addition, the external carry means that a missile in the airstream is exposed to temperatures of about -65 F. Missiles and missile components therefore are subject to temperatures from -65 F to well over 300 F. |
| format | Report |
| fullrecord | <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_AD0513348</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>AD0513348</sourcerecordid><originalsourceid>FETCH-dtic_stinet_AD05133483</originalsourceid><addsrcrecordid>eNrjZNAKyUgtyk3MyalUCC5JTMpJVXAqLcrLzEtXCEosSVVwTE5OzUktSizJLyrmYWBNS8wpTuWF0twMMm6uIc4euiklmcnxxSWZeakl8Y4uBqaGxsYmFsYEpAGESCXh</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Thermally Stable Burning Rate Accelerators</title><source>DTIC Technical Reports</source><creator>Stephens, W D ; Flanigan, D A ; Hightower, J O ; Miller, M ; Willis, T C</creator><creatorcontrib>Stephens, W D ; Flanigan, D A ; Hightower, J O ; Miller, M ; Willis, T C ; MORTON THIOKOL INC HUNTSVILLE AL HUNTSVILLE DIV</creatorcontrib><description>The purpose of this program is to research the methods and materials that will produce thermally stable AP and burning rate catalyst. They will be used with other thermally stable propellant ingredients to produce a solid propellant that is capable of withstanding a temperature environment of -75 to 350 F. With the present capability of aircraft to fly at supersonic speeds, a new requirement now exists for missiles which can be carried externally. The major development problem arises from the effects of aerodynamic heating, causing missile skin temperatures of several hundred degrees Fahrenheit. In addition, the external carry means that a missile in the airstream is exposed to temperatures of about -65 F. Missiles and missile components therefore are subject to temperatures from -65 F to well over 300 F.</description><language>eng</language><subject>ACETIC ACID ; ADDITIVES ; AERODYNAMIC CHARACTERISTICS ; ALUMINUM COMPOUNDS ; AMMONIUM PERCHLORATE ; ANHYDRIDES ; AROMATIC COMPOUNDS ; BALLISTIC MODIFIERS ; BURNING RATE ; CATALYSTS ; CHEMICAL MILLING ; CHLORIDES ; Combustion and Ignition ; CRYSTAL LATTICES ; FERROCENES ; FERROCENYL PROPELLANT INGREDIENTS ; FREEZE DRYING ; GRINDING ; GUIDED MISSILES ; HEAT SHIELDS ; HUMIDITY ; HYDROLYSIS ; INTERIOR BALLISTICS ; PARTICLE SIZE ; POLYMERS ; PURIFICATION ; RECRYSTALLIZATION (U) SOLID ROCKET PROPELLANTS ; REDUCTION ; ROCKET ENGINE CASES ; ROCKET MOTORS(SOLID PROPELLANT) ; SOLID ROCKET OXIDIZERS ; Solid Rocket Propellants ; SPRAY DRYING ; SPRAYS ; SUBLIMATION ; THERMAL INSULATION ; THERMAL STABILITY ; UFAPULTRAFINE AMMONIUM PERCHLORATE ; ULTRAFINES ; ULTRASONIC RADIATION</subject><creationdate>1971</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>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0513348$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Stephens, W D</creatorcontrib><creatorcontrib>Flanigan, D A</creatorcontrib><creatorcontrib>Hightower, J O</creatorcontrib><creatorcontrib>Miller, M</creatorcontrib><creatorcontrib>Willis, T C</creatorcontrib><creatorcontrib>MORTON THIOKOL INC HUNTSVILLE AL HUNTSVILLE DIV</creatorcontrib><title>Thermally Stable Burning Rate Accelerators</title><description>The purpose of this program is to research the methods and materials that will produce thermally stable AP and burning rate catalyst. They will be used with other thermally stable propellant ingredients to produce a solid propellant that is capable of withstanding a temperature environment of -75 to 350 F. With the present capability of aircraft to fly at supersonic speeds, a new requirement now exists for missiles which can be carried externally. The major development problem arises from the effects of aerodynamic heating, causing missile skin temperatures of several hundred degrees Fahrenheit. In addition, the external carry means that a missile in the airstream is exposed to temperatures of about -65 F. Missiles and missile components therefore are subject to temperatures from -65 F to well over 300 F.</description><subject>ACETIC ACID</subject><subject>ADDITIVES</subject><subject>AERODYNAMIC CHARACTERISTICS</subject><subject>ALUMINUM COMPOUNDS</subject><subject>AMMONIUM PERCHLORATE</subject><subject>ANHYDRIDES</subject><subject>AROMATIC COMPOUNDS</subject><subject>BALLISTIC MODIFIERS</subject><subject>BURNING RATE</subject><subject>CATALYSTS</subject><subject>CHEMICAL MILLING</subject><subject>CHLORIDES</subject><subject>Combustion and Ignition</subject><subject>CRYSTAL LATTICES</subject><subject>FERROCENES</subject><subject>FERROCENYL PROPELLANT INGREDIENTS</subject><subject>FREEZE DRYING</subject><subject>GRINDING</subject><subject>GUIDED MISSILES</subject><subject>HEAT SHIELDS</subject><subject>HUMIDITY</subject><subject>HYDROLYSIS</subject><subject>INTERIOR BALLISTICS</subject><subject>PARTICLE SIZE</subject><subject>POLYMERS</subject><subject>PURIFICATION</subject><subject>RECRYSTALLIZATION (U) SOLID ROCKET PROPELLANTS</subject><subject>REDUCTION</subject><subject>ROCKET ENGINE CASES</subject><subject>ROCKET MOTORS(SOLID PROPELLANT)</subject><subject>SOLID ROCKET OXIDIZERS</subject><subject>Solid Rocket Propellants</subject><subject>SPRAY DRYING</subject><subject>SPRAYS</subject><subject>SUBLIMATION</subject><subject>THERMAL INSULATION</subject><subject>THERMAL STABILITY</subject><subject>UFAPULTRAFINE AMMONIUM PERCHLORATE</subject><subject>ULTRAFINES</subject><subject>ULTRASONIC RADIATION</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1971</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZNAKyUgtyk3MyalUCC5JTMpJVXAqLcrLzEtXCEosSVVwTE5OzUktSizJLyrmYWBNS8wpTuWF0twMMm6uIc4euiklmcnxxSWZeakl8Y4uBqaGxsYmFsYEpAGESCXh</recordid><startdate>197101</startdate><enddate>197101</enddate><creator>Stephens, W D</creator><creator>Flanigan, D A</creator><creator>Hightower, J O</creator><creator>Miller, M</creator><creator>Willis, T C</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>197101</creationdate><title>Thermally Stable Burning Rate Accelerators</title><author>Stephens, W D ; Flanigan, D A ; Hightower, J O ; Miller, M ; Willis, T C</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD05133483</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1971</creationdate><topic>ACETIC ACID</topic><topic>ADDITIVES</topic><topic>AERODYNAMIC CHARACTERISTICS</topic><topic>ALUMINUM COMPOUNDS</topic><topic>AMMONIUM PERCHLORATE</topic><topic>ANHYDRIDES</topic><topic>AROMATIC COMPOUNDS</topic><topic>BALLISTIC MODIFIERS</topic><topic>BURNING RATE</topic><topic>CATALYSTS</topic><topic>CHEMICAL MILLING</topic><topic>CHLORIDES</topic><topic>Combustion and Ignition</topic><topic>CRYSTAL LATTICES</topic><topic>FERROCENES</topic><topic>FERROCENYL PROPELLANT INGREDIENTS</topic><topic>FREEZE DRYING</topic><topic>GRINDING</topic><topic>GUIDED MISSILES</topic><topic>HEAT SHIELDS</topic><topic>HUMIDITY</topic><topic>HYDROLYSIS</topic><topic>INTERIOR BALLISTICS</topic><topic>PARTICLE SIZE</topic><topic>POLYMERS</topic><topic>PURIFICATION</topic><topic>RECRYSTALLIZATION (U) SOLID ROCKET PROPELLANTS</topic><topic>REDUCTION</topic><topic>ROCKET ENGINE CASES</topic><topic>ROCKET MOTORS(SOLID PROPELLANT)</topic><topic>SOLID ROCKET OXIDIZERS</topic><topic>Solid Rocket Propellants</topic><topic>SPRAY DRYING</topic><topic>SPRAYS</topic><topic>SUBLIMATION</topic><topic>THERMAL INSULATION</topic><topic>THERMAL STABILITY</topic><topic>UFAPULTRAFINE AMMONIUM PERCHLORATE</topic><topic>ULTRAFINES</topic><topic>ULTRASONIC RADIATION</topic><toplevel>online_resources</toplevel><creatorcontrib>Stephens, W D</creatorcontrib><creatorcontrib>Flanigan, D A</creatorcontrib><creatorcontrib>Hightower, J O</creatorcontrib><creatorcontrib>Miller, M</creatorcontrib><creatorcontrib>Willis, T C</creatorcontrib><creatorcontrib>MORTON THIOKOL INC HUNTSVILLE AL HUNTSVILLE DIV</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Stephens, W D</au><au>Flanigan, D A</au><au>Hightower, J O</au><au>Miller, M</au><au>Willis, T C</au><aucorp>MORTON THIOKOL INC HUNTSVILLE AL HUNTSVILLE DIV</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Thermally Stable Burning Rate Accelerators</btitle><date>1971-01</date><risdate>1971</risdate><abstract>The purpose of this program is to research the methods and materials that will produce thermally stable AP and burning rate catalyst. They will be used with other thermally stable propellant ingredients to produce a solid propellant that is capable of withstanding a temperature environment of -75 to 350 F. With the present capability of aircraft to fly at supersonic speeds, a new requirement now exists for missiles which can be carried externally. The major development problem arises from the effects of aerodynamic heating, causing missile skin temperatures of several hundred degrees Fahrenheit. In addition, the external carry means that a missile in the airstream is exposed to temperatures of about -65 F. Missiles and missile components therefore are subject to temperatures from -65 F to well over 300 F.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_dtic_stinet_AD0513348 |
| source | DTIC Technical Reports |
| subjects | ACETIC ACID ADDITIVES AERODYNAMIC CHARACTERISTICS ALUMINUM COMPOUNDS AMMONIUM PERCHLORATE ANHYDRIDES AROMATIC COMPOUNDS BALLISTIC MODIFIERS BURNING RATE CATALYSTS CHEMICAL MILLING CHLORIDES Combustion and Ignition CRYSTAL LATTICES FERROCENES FERROCENYL PROPELLANT INGREDIENTS FREEZE DRYING GRINDING GUIDED MISSILES HEAT SHIELDS HUMIDITY HYDROLYSIS INTERIOR BALLISTICS PARTICLE SIZE POLYMERS PURIFICATION RECRYSTALLIZATION (U) SOLID ROCKET PROPELLANTS REDUCTION ROCKET ENGINE CASES ROCKET MOTORS(SOLID PROPELLANT) SOLID ROCKET OXIDIZERS Solid Rocket Propellants SPRAY DRYING SPRAYS SUBLIMATION THERMAL INSULATION THERMAL STABILITY UFAPULTRAFINE AMMONIUM PERCHLORATE ULTRAFINES ULTRASONIC RADIATION |
| title | Thermally Stable Burning Rate Accelerators |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-13T00%3A08%3A27IST&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=Thermally%20Stable%20Burning%20Rate%20Accelerators&rft.au=Stephens,%20W%20D&rft.aucorp=MORTON%20THIOKOL%20INC%20HUNTSVILLE%20AL%20HUNTSVILLE%20DIV&rft.date=1971-01&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EAD0513348%3C/dtic_1RU%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |