Results 101 to 110 of about 449 (191)

Hydroxy-terminated polyether binders for composite rocket propellants

open access: yes, 2007
Propellants based on cross-linked Hydroxy Terminated PolyEther (HTPE) binders are being used as alternatives to Hydroxy Terminated PolyButadiene (HTPB) compositions. HTPE propellants have similar mechanical properties to HTPB propellants but they give a less severe response in ‘slow cook-off’ tests for IM compliance. A literature review is presented on
openaire   +1 more source

Composite Solid Rocket Propellant Aging: Multi Parameter Statistical Analysis

open access: yesInternational Journal of Aeronautics and Aerospace Engineering, 2022
openaire   +1 more source

Study on Composite Solid Propellants for Rocket Assisted Projectile

open access: yesJournal of the Korean Society for Aeronautical & Space Sciences, 2010
Kyung-Moo Kim   +2 more
openaire   +2 more sources

Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]

open access: yesPolymers (Basel)
Chmielarek M   +2 more
europepmc   +1 more source

Thermal Insulation Based on NBR-Elastomerized Phenolic Resin Reinforced with Carbon Fibers: Mechanical and Ablation Properties. [PDF]

open access: yesMaterials (Basel)
Gržetić J   +6 more
europepmc   +1 more source

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