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Assessment of analytical techniques for predicting solid propellant exhaust plumes and plume impingement environments [PDF]

An analysis of experimental nozzle, exhaust plume, and exhaust plume impingement data is presented. The data were obtained for subscale solid propellant motors with propellant Al loadings of 2, 10 and 15% exhausting to simulated altitudes of 50,000, 100 ...
Penny, M. M., Smith, S. D., Tevepaugh, J. A. +2 more
core +1 more source

Biodegradability of Binder System Waste from Hydroxyl-Terminated Polybutadiene Propellant and Pretreatment for Biodegradation. [PDF]

Polymers (Basel)
Wu K, Chai T, Hu F, Ding Z, Wang C.
europepmc +1 more source

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

Polymers (Basel)
Chmielarek M, Szczęśniak B, Blacharski K. +2 more
europepmc +1 more source

Status of Propulsion Technology Development Under the NASA In-space Propulsion Technology Program [PDF]

Since 2001, the In-Space Propulsion Technology (ISPT) program has been developing and delivering in-space propulsion technologies for NASA's Science Mission Directorate (SMD).
Anderson, David +5 more
core +1 more source

Numerical Simulation of Failure Modes of Solid Propellants with Internal Cavities Under Various Loading Conditions. [PDF]

Polymers (Basel)
Liu K, Yang Q, Cao L, Wang J, Cao P.
europepmc +1 more source

Study on Mechanical Properties and Failure Mechanisms of Highly Filled Hydroxy-Terminated Polybutadiene Propellant under Different Tensile Loading Conditions. [PDF]