Solid Propellant Temperature Profiles Obtained through Embedded Microthermocouples

This report presents the results acquired during a solid propellant combustion project at the Astronautics Laboratory from 1/90-7/90. Four propellants were studied: Ammonium nitrate (primarily), double base, HMX1, and HMX2. The results are presented as temperature profiles of the various propellants...

Full description

Saved in:
Bibliographic Details
Main Author: Hall, Gregory M
Format: Report
Language:English
Subjects:
AMMONIUM NITRATE
AMMONIUM NITRATES
ANGLES
ASTRONAUTICS
COMBUSTION
Combustion and Ignition
DOUBLE BASED PROPELLANTS
EMBEDDING
HMX
LABORATORIES
PE62302F
PROFILES
PROPELLANTS
SIZES(DIMENSIONS)
SOLID PROPELLANTS
Solid Rocket Propellants
TEMPERATURE
THERMOCOUPLES
WUAL573000Q3
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 Hall, Gregory M
description This report presents the results acquired during a solid propellant combustion project at the Astronautics Laboratory from 1/90-7/90. Four propellants were studied: Ammonium nitrate (primarily), double base, HMX1, and HMX2. The results are presented as temperature profiles of the various propellants. These were obtained through the use of embedded thermocouples in the propellants. In addition to temperature profiles, different thermocouple sizes and lead angles, different embedment processes, and observations of the burn characteristics are all included as data.
format report
fullrecord <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_ADA229975</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ADA229975</sourcerecordid><originalsourceid>FETCH-dtic_stinet_ADA2299753</originalsourceid><addsrcrecordid>eNrjZAgKzs_JTFEIKMovSM3JScwrUQhJzS1ILUosKS1KBQmnZeakFiv4J5UkZualpiiUZBTll6ZnKLjmJqWmpAAFfDOTi_JLMlKLcvOT80sLgIp5GFjTEnOKU3mhNDeDjJtriLOHbkpJZnJ8cQnQnJJ4RxdHIyNLS3NTYwLSADKDNfw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Solid Propellant Temperature Profiles Obtained through Embedded Microthermocouples</title><source>DTIC Technical Reports</source><creator>Hall, Gregory M</creator><creatorcontrib>Hall, Gregory M ; EDWARDS AFB CA</creatorcontrib><description>This report presents the results acquired during a solid propellant combustion project at the Astronautics Laboratory from 1/90-7/90. Four propellants were studied: Ammonium nitrate (primarily), double base, HMX1, and HMX2. The results are presented as temperature profiles of the various propellants. These were obtained through the use of embedded thermocouples in the propellants. In addition to temperature profiles, different thermocouple sizes and lead angles, different embedment processes, and observations of the burn characteristics are all included as data.</description><language>eng</language><subject>AMMONIUM NITRATE ; AMMONIUM NITRATES ; ANGLES ; ASTRONAUTICS ; COMBUSTION ; Combustion and Ignition ; DOUBLE BASED PROPELLANTS ; EMBEDDING ; HMX ; LABORATORIES ; PE62302F ; PROFILES ; PROPELLANTS ; SIZES(DIMENSIONS) ; SOLID PROPELLANTS ; Solid Rocket Propellants ; TEMPERATURE ; THERMOCOUPLES ; WUAL573000Q3</subject><creationdate>1990</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/ADA229975$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Hall, Gregory M</creatorcontrib><creatorcontrib>EDWARDS AFB CA</creatorcontrib><title>Solid Propellant Temperature Profiles Obtained through Embedded Microthermocouples</title><description>This report presents the results acquired during a solid propellant combustion project at the Astronautics Laboratory from 1/90-7/90. Four propellants were studied: Ammonium nitrate (primarily), double base, HMX1, and HMX2. The results are presented as temperature profiles of the various propellants. These were obtained through the use of embedded thermocouples in the propellants. In addition to temperature profiles, different thermocouple sizes and lead angles, different embedment processes, and observations of the burn characteristics are all included as data.</description><subject>AMMONIUM NITRATE</subject><subject>AMMONIUM NITRATES</subject><subject>ANGLES</subject><subject>ASTRONAUTICS</subject><subject>COMBUSTION</subject><subject>Combustion and Ignition</subject><subject>DOUBLE BASED PROPELLANTS</subject><subject>EMBEDDING</subject><subject>HMX</subject><subject>LABORATORIES</subject><subject>PE62302F</subject><subject>PROFILES</subject><subject>PROPELLANTS</subject><subject>SIZES(DIMENSIONS)</subject><subject>SOLID PROPELLANTS</subject><subject>Solid Rocket Propellants</subject><subject>TEMPERATURE</subject><subject>THERMOCOUPLES</subject><subject>WUAL573000Q3</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1990</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZAgKzs_JTFEIKMovSM3JScwrUQhJzS1ILUosKS1KBQmnZeakFiv4J5UkZualpiiUZBTll6ZnKLjmJqWmpAAFfDOTi_JLMlKLcvOT80sLgIp5GFjTEnOKU3mhNDeDjJtriLOHbkpJZnJ8cQnQnJJ4RxdHIyNLS3NTYwLSADKDNfw</recordid><startdate>199010</startdate><enddate>199010</enddate><creator>Hall, Gregory M</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>199010</creationdate><title>Solid Propellant Temperature Profiles Obtained through Embedded Microthermocouples</title><author>Hall, Gregory M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA2299753</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1990</creationdate><topic>AMMONIUM NITRATE</topic><topic>AMMONIUM NITRATES</topic><topic>ANGLES</topic><topic>ASTRONAUTICS</topic><topic>COMBUSTION</topic><topic>Combustion and Ignition</topic><topic>DOUBLE BASED PROPELLANTS</topic><topic>EMBEDDING</topic><topic>HMX</topic><topic>LABORATORIES</topic><topic>PE62302F</topic><topic>PROFILES</topic><topic>PROPELLANTS</topic><topic>SIZES(DIMENSIONS)</topic><topic>SOLID PROPELLANTS</topic><topic>Solid Rocket Propellants</topic><topic>TEMPERATURE</topic><topic>THERMOCOUPLES</topic><topic>WUAL573000Q3</topic><toplevel>online_resources</toplevel><creatorcontrib>Hall, Gregory M</creatorcontrib><creatorcontrib>EDWARDS AFB CA</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Hall, Gregory M</au><aucorp>EDWARDS AFB CA</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Solid Propellant Temperature Profiles Obtained through Embedded Microthermocouples</btitle><date>1990-10</date><risdate>1990</risdate><abstract>This report presents the results acquired during a solid propellant combustion project at the Astronautics Laboratory from 1/90-7/90. Four propellants were studied: Ammonium nitrate (primarily), double base, HMX1, and HMX2. The results are presented as temperature profiles of the various propellants. These were obtained through the use of embedded thermocouples in the propellants. In addition to temperature profiles, different thermocouple sizes and lead angles, different embedment processes, and observations of the burn characteristics are all included as data.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_dtic_stinet_ADA229975
source DTIC Technical Reports
subjects AMMONIUM NITRATE
AMMONIUM NITRATES
ANGLES
ASTRONAUTICS
COMBUSTION
Combustion and Ignition
DOUBLE BASED PROPELLANTS
EMBEDDING
HMX
LABORATORIES
PE62302F
PROFILES
PROPELLANTS
SIZES(DIMENSIONS)
SOLID PROPELLANTS
Solid Rocket Propellants
TEMPERATURE
THERMOCOUPLES
WUAL573000Q3
title Solid Propellant Temperature Profiles Obtained through Embedded Microthermocouples
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T18%3A37%3A56IST&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=Solid%20Propellant%20Temperature%20Profiles%20Obtained%20through%20Embedded%20Microthermocouples&rft.au=Hall,%20Gregory%20M&rft.aucorp=EDWARDS%20AFB%20CA&rft.date=1990-10&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EADA229975%3C/dtic_1RU%3E%3Cgrp_id%3Ecdi_FETCH-dtic_stinet_ADA2299753%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