Multiple Diagnostics of Hybrid Rocket Ignition and Effect of Hypergolic Additive Granulometry
Hybrid-Propellant Power Plant (Section 3.5)
Burning Rate Optimization Under Uncertainty Using Response Surfaces and Monte Carlo Simulation
Advanced Cryogenic Solid Hybrid Rocket Engine Developments: Concept and Test Results
Biphasic Dispersion Fuels for High-Regression-Rate Hybrid Rockets
Investigation of a Marine Water-Breathing Hybrid Ram-Rocket Motor
Reducing the Ignition Delay of Hypergolic Hybrid Rocket Fuels
Mars Ascent Vehicle Hybrid PropulsionEffort
Mars Ascent Vehicle Hybrid Propulsion Effort
Conceptual Study on Low-Melting-Point Thermoplastic Fuel/Nitrous Oxide Hybrid Rockoon
Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage
Development of a Power-Efficient, Restart-Capable Arc Ignitor for Hybrid Rockets
Returning Geological Samples from Mars
Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure
Ignition and Combustion Enhancement of Boron with Polytetrafluoroethylene
Autoignitable and Restartable Hybrid Rockets Using Catalytic Decomposition of an Oxidizer
Plume Contamination Measurements of an Additively Printed, Green-Propellant Hybrid Thruster
Enhancement of Hybrid Fuel Regression Rate Using a Bluff Body
Experimental Investigation of Prepackaged Hybrid Propulsion Systems
Issues Related to the Measurement of Regression Rate of Fast-Burning Hybrid Fuels
Ballistic Performance of Paraffin-Based Solid Fuels Enhanced by Catalytic Polymer Degradation
Preliminary Assessment of Using Gelled and Hybrid Propellant Propulsion for VTOL/SSTO Launch Systems
Characterization of Ethylenediamine Bisborane as a Hypergolic Hybrid Rocket Fuel Additive
Additive Manufacturing of Solid Rocket Propellant Grains
Mars Ascent Vehicle Hybrid PropulsionEffort
Mars Ascent Vehicle Hybrid Propulsion Effort
Rockets and Astronautics. (Lexicon Contribution) Raketen und Raumfahrt. (Beitraege fuer Lexikon)
Three-Dimensional Printing of “Green” Fuels for Low-Cost Small Spacecraft Propulsion Systems
Theoretical Performance of the Hybrid Rocket Propellant Combination F L O X/ Polyethylene
Nitrous Oxide and Oxygen Mixtures (Nytrox) as Oxidizers for Rocket Propulsion Applications
A Miniaturized, Green, End-Burning, and Sandwich Hybrid Propulsion System
Large-Scale Hybrid Motor Performance and Designs for Use in Launch Vehicle Applications
Survey of Selected Additively Manufactured Propellants for Arc Ignition of Hybrid Rockets
Propergols Hautement Energetiques (High Energy Propellants)
The Solid-Liquid Rocket Engine
Some Typical Hybrid Propellant Rocket Motors
Radiation Heating Effects on Oxidizer-to-Fuel Ratio of Additively Manufactured Hybrid Rocket Fuels
JANNAF Propulsion Meeting, 1990. Volume 2. Held in Anaheim, California on October 3-5, 1990
Deep Throttle of a Nitrous Oxide and Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor
Thermochemical Ablation of Rocket Nozzle Insert Materials Final Report
Large-Scale Hybrid Motor Testing, Chapter 10
Engineering Model for Hybrid Fuel Regression Rate Amplification Using Helical Ports
Hybrid Rocket Combustion Regression Rate Model
Hybrid Propulsion Technology Program: Phase 1, Volume 4