A Method for Reducing the Temperature Sensitivity of a Single-Base Propellant by Adding Ultra-Fine RDX Particles. [PDF]
Zhu S +9 more
europepmc +1 more source
Estimating CO2 emissions due to present and future suborbital space tourism industry. [PDF]
Huang AM, Xu Y.
europepmc +1 more source
Interrelation Between Dilatation Rate and Displacement Speed in Premixed Turbulent Flames. [PDF]
Mohan V +4 more
europepmc +1 more source
Design of an onboard computer for small experimental rockets with an integrated hardware-in-the-loop validation framework. [PDF]
Netzel NA +4 more
europepmc +1 more source
Progress and Bottlenecks in Large-Scale Commercial Space Transportation Systems. [PDF]
Wang X, Song Z, Bao W.
europepmc +1 more source
Elucidating the Gas Phase Thermochemistry and the H‑Atom Abstraction Reactions of Triethyl Phosphite. [PDF]
Zhu Z +8 more
europepmc +1 more source
Advanced Design Concepts for Ceramic Thrust Chamber Components of Rocket Engines [PDF]
Ortelt, Markus +3 more
core
A DFT Study of the Reaction Products/Mechanism in Plasma-Assisted Ammonia Synthesis from Water and Nitrogen and Their Infrared Analysis. [PDF]
Zeinalipour-Yazdi CD, Wang X.
europepmc +1 more source
Amine-AlH<sub>3</sub> Adducts as Energetic Materials for a New Generation of Solid Fuels. [PDF]
Liu X +4 more
europepmc +1 more source

