Solid smokeless propellants and pyrotechnic compositions for rocket and gas generation systems
Solid gas generant compositions produce low particulates of the slightly-soluble or insoluble type when combusted. More specifically the solid gas generants and/or ignition compositions are provided which include an effective combination of phase stabilized ammonium nitrate (PSAN) as a oxidizer comp...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Patent |
Sprache: | eng |
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 | Scheffee, Robert Lundstrom, Norman |
description | Solid gas generant compositions produce low particulates of the slightly-soluble or insoluble type when combusted. More specifically the solid gas generants and/or ignition compositions are provided which include an effective combination of phase stabilized ammonium nitrate (PSAN) as a oxidizer component and azodiformamidine dinitrate (AZODN) as the fuel component. Most preferably, the AN is phase stabilized with a phase stabilizing effective amount of a phase stabilizer selected from potassium perchlorate (KP) and/or potassium nitrate (KN). |
format | Patent |
fullrecord | <record><control><sourceid>uspatents_EFI</sourceid><recordid>TN_cdi_uspatents_applications_20020195181</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>20020195181</sourcerecordid><originalsourceid>FETCH-uspatents_applications_200201951813</originalsourceid><addsrcrecordid>eNqVjTEKwkAQRdNYiHqHaS2EJCJoLYq91oZhM9Elm51h_1rk9mrwAlav-O_z5sX9qsG3hEF7CQKQJTUJgWMGcWzJxqRZ3DN6R04HU_jsNYI6TZTU9ZIn78Ggh0RJ_J0JI7IMWBazjgNk9eOiWJ9Pt-Nl84Jxlk-kYbPg3fRCU5dlXVaHXbWvtv-4b067RLc</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Solid smokeless propellants and pyrotechnic compositions for rocket and gas generation systems</title><source>USPTO Published Applications</source><creator>Scheffee, Robert ; Lundstrom, Norman</creator><creatorcontrib>Scheffee, Robert ; Lundstrom, Norman</creatorcontrib><description>Solid gas generant compositions produce low particulates of the slightly-soluble or insoluble type when combusted. More specifically the solid gas generants and/or ignition compositions are provided which include an effective combination of phase stabilized ammonium nitrate (PSAN) as a oxidizer component and azodiformamidine dinitrate (AZODN) as the fuel component. Most preferably, the AN is phase stabilized with a phase stabilizing effective amount of a phase stabilizer selected from potassium perchlorate (KP) and/or potassium nitrate (KN).</description><language>eng</language><creationdate>2002</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20020195181$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,778,871,883,64044</link.rule.ids><linktorsrc>$$Uhttps://patentcenter.uspto.gov/applications/09871713$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Scheffee, Robert</creatorcontrib><creatorcontrib>Lundstrom, Norman</creatorcontrib><title>Solid smokeless propellants and pyrotechnic compositions for rocket and gas generation systems</title><description>Solid gas generant compositions produce low particulates of the slightly-soluble or insoluble type when combusted. More specifically the solid gas generants and/or ignition compositions are provided which include an effective combination of phase stabilized ammonium nitrate (PSAN) as a oxidizer component and azodiformamidine dinitrate (AZODN) as the fuel component. Most preferably, the AN is phase stabilized with a phase stabilizing effective amount of a phase stabilizer selected from potassium perchlorate (KP) and/or potassium nitrate (KN).</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2002</creationdate><recordtype>patent</recordtype><sourceid>EFI</sourceid><recordid>eNqVjTEKwkAQRdNYiHqHaS2EJCJoLYq91oZhM9Elm51h_1rk9mrwAlav-O_z5sX9qsG3hEF7CQKQJTUJgWMGcWzJxqRZ3DN6R04HU_jsNYI6TZTU9ZIn78Ggh0RJ_J0JI7IMWBazjgNk9eOiWJ9Pt-Nl84Jxlk-kYbPg3fRCU5dlXVaHXbWvtv-4b067RLc</recordid><startdate>20021226</startdate><enddate>20021226</enddate><creator>Scheffee, Robert</creator><creator>Lundstrom, Norman</creator><scope>EFI</scope></search><sort><creationdate>20021226</creationdate><title>Solid smokeless propellants and pyrotechnic compositions for rocket and gas generation systems</title><author>Scheffee, Robert ; Lundstrom, Norman</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_applications_200201951813</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2002</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Scheffee, Robert</creatorcontrib><creatorcontrib>Lundstrom, Norman</creatorcontrib><collection>USPTO Published Applications</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Scheffee, Robert</au><au>Lundstrom, Norman</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Solid smokeless propellants and pyrotechnic compositions for rocket and gas generation systems</title><date>2002-12-26</date><risdate>2002</risdate><abstract>Solid gas generant compositions produce low particulates of the slightly-soluble or insoluble type when combusted. More specifically the solid gas generants and/or ignition compositions are provided which include an effective combination of phase stabilized ammonium nitrate (PSAN) as a oxidizer component and azodiformamidine dinitrate (AZODN) as the fuel component. Most preferably, the AN is phase stabilized with a phase stabilizing effective amount of a phase stabilizer selected from potassium perchlorate (KP) and/or potassium nitrate (KN).</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_uspatents_applications_20020195181 |
source | USPTO Published Applications |
title | Solid smokeless propellants and pyrotechnic compositions for rocket and gas generation systems |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-15T23%3A05%3A49IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-uspatents_EFI&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Scheffee,%20Robert&rft.date=2002-12-26&rft_id=info:doi/&rft_dat=%3Cuspatents_EFI%3E20020195181%3C/uspatents_EFI%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 |