Solid Propellant Structural Integrity Investigations: Dynamic Response and Failure Mechanisms. Quarterly Progress Report No. 2

Item

Title
Solid Propellant Structural Integrity Investigations: Dynamic Response and Failure Mechanisms. Quarterly Progress Report No. 2
Date
1965
Index Abstract
Not Available
Photo Quality
Undetermined
Report Number
AFRPL TR 65-20
Creator
Cantey, D. E.
Corporate Author
Lockheed Propulsion Company
Laboratory
Air Force Rocket Propulsion Laboratory
Date Issued
1965-01-15
Extent
87
Identifier
AD0610615
Access Rights
Unknown
Distribution Classification
1
Contract
AF 04(611)-9953
DoD Project
3059
DoD Task
None Given
DTIC Record Exists
Yes
Distribution Change Authority Correspondence
None
Distribution Conflict
No
Abstract
The results of an investigation of viscoelastic and failure properties of highly filled PBAA and PBAN propellants as a function of solids loading are reported. Failure surface study results are reported, and the results of a limited study of the relationship between crack propagation velocity and propellant physical characteristics are discussed. Propellant dynamic shear and bulk properties were investigated with small deformation piezoelectric devices. An experimental investigation of propellant thermomechanical response to sustained cyclic inertial loading was completed, and the results in agreement with theory are presented. Also discussed are experimental investigations of transient thermoviscoelastic response of propellant under constant cyclic strain amplitude and inertial loading.
Report Availability
Not available via Contrails
Index In
DTIC
Type
report

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