Results 101 to 110 of about 1,271 (200)

Large-Scale Hybrid Motor Testing [PDF]

open access: yes
Hybrid rocket motors can be successfully demonstrated at a small scale virtually anywhere. There have been many suitcase sized portable test stands assembled for demonstration of hybrids. They show the safety of hybrid rockets to the audiences.
Story, George
core   +1 more source

Studying the influence of aluminium in ADN/HTPB-based solid propellants [PDF]

open access: yes
Ammonium Dinitramide (ADN) combustion has been the subject of great interest over the past few years due to consideration as a green oxidizer in solid rocket propellants.
Kore, Rushikesh   +2 more
core   +1 more source

Effect of Curing Parameter on the Mechanical Properties and Bond Strength at Propellant-Liner Interfaces in Rocket Motors

open access: yesChemical Engineering Transactions
This study investigates the effect of curing parameters (Rt) on the mechanical properties and bond strength of propellants and liners in rocket motors compared to the design values.
Thirapat Kitinirunkul   +3 more
doaj  

Hybrid propulsion technology program: Phase 1. Volume 3: Thiokol Corporation Space Operations [PDF]

open access: yes
Three candidate hybrid propulsion (HP) concepts were identified, optimized, evaluated, and refined through an iterative process that continually forced improvement to the systems with respect to safety, reliability, cost, and performance criteria. A full
Schuler, A. L., Wiley, D. R.
core   +1 more source

Combustion chemistry of solid propellants [PDF]

open access: yes
Several studies are described of the chemistry of solid propellant combustion which employed a fast-scanning optical spectrometer. Expanded abstracts are presented for four of the studies which were previously reported.
Baer, A. D., Ryan, N. W.
core   +1 more source

Catalyst Screening for Ammonium Nitrate Oxidizer [PDF]

open access: yes, 2017
Arosio, L., Galfetti, L., Maggi, F.
core   +1 more source

Hybrid Propulsion Technology Program [PDF]

open access: yes
Future launch systems of the United States will require improvements in booster safety, reliability, and cost. In order to increase payload capabilities, performance improvements are also desirable.
Holzman, A. L., Jensen, G. E.
core   +1 more source

Plasticizer-Enabled Solvent-Free Curing of Self-Healing Binder System for Energetic Materials. [PDF]

open access: yesPolymers (Basel)
Zhang M   +9 more
europepmc   +1 more source

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

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

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