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...

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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
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Summary: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.