Results 41 to 50 of about 1,166 (199)
Ballistic effectiveness of Zr-containing composite solid propellants as a function of binder nature and mass fraction [PDF]
This paper considers the effects of binder mass fraction on the properties of energetic formulations based on zirconium and zirconium hydride. These ingredients, replacing aluminum in solid rocket motors with low vehicle performance coefficient, may ...
D. B. Lempert +2 more
core +2 more sources
Abstract The fluffy fibers based on nitrocellulose (NC)/ammonium dinitramide (ADN) with high explosives have been fabricated by electrospinning technique. The morphology, thermal stability, combustion behaviors and mechanical sensitivity of NC/ADN-based composite fibers were characterized by means of scanning electron microscope (SEM ...
Qiong Wang +5 more
openaire +1 more source
Achieving Balanced Energetics through Cocrystallization [PDF]
Achieving energetic materials with a balanced ratio of oxidant to fuel is a challenge that has been difficult to meet through molecular synthesis. The alternative approach, composite formulation, fails to achieve intimate association of the components to
Bellas, Michael K., Matzger, Adam J.
core +2 more sources
Additive Manufacturing of Ceramic Materials: a Performance Comparison of Catalysts for Monopropellant Thrusters [PDF]
Switchgrass ( L.) is a promising herbaceous energy crop, but further gains in biomass yield and quality must be achieved to enable a viable bioenergy industry.
Aruna Nandety +7 more
core +2 more sources
Thermal Ignition of ADN‐Based Propellants
Abstract Ammonium dinitramide (ADN, NH4+ N(NO2)2−) based monopropellants are extremely promising as hydrazine replacement. Thermal igniters are attractive for ADN thrusters as they allow a more prompt ignition and may be better suited for larger engines (100‐500 N) compared to the currently used preheated catalysts.
Michele Negri +2 more
wiley +1 more source
Ammonium dinitramide (ADN) and 3,4‐Diaminofurazan (DAF) form a 1:1 energetic cocrystal. We report its crystal structure and spectroscopic signature and evaluate thermal stability, decomposition behavior, hygroscopicity, and combustion properties. Propellant performance calculations benchmark the material against guanylurea dinitramide (GuDN) and ...
Peter Schultz +2 more
wiley +1 more source
Click and cross: A novel azide terminated ethylene oxide‐tetrahydrofuran copolymer with urethane segments (ATUPET) has been prepared through a facile method. The elastomers based on ATUPET exhibited improved mechanical properties and satisfactory thermal stability, which indicated that this might be a promising polymeric binder for future propellant ...
Qian Zhang +6 more
wiley +1 more source
From Lampoldshausen to Space: DLR Spin-off InSpacePropulsion Technologies and the Development Status of Green Propellant Thrusters Based on H2O2 and N2O [PDF]
The German Aerospace Center’s Institute of Space Propulsion in Lampoldshausen has more than a decade of experience in green propellant research and green propulsion hardware development.
Braune, Luca +8 more
core +1 more source
ABSTRACT The aerospace industry is continually seeking materials that offer higher performance and lower environmental impact. In chemical propulsion, ammonium dinitramide (ADN) represents a significant advance in this direction as a potential replacement for ammonium perchlorate in solid propellant formulations.
Josiane R. C. Silva +6 more
wiley +1 more source
Research Progresses of Flash Evaporation in Aerospace Applications
Liquid is overheated and evaporated quickly when it enters into the environment with lower saturation pressure than that corresponding to its initial temperature. This phenomenon is known as the flash evaporation. A natural low‐pressure environment and flash evaporation have unique characteristics and superiority in high altitude and outer space ...
Wei Ma +9 more
wiley +1 more source

