Demilitarisation of Lance Rocket Motors
Clean Propellants for Space Launch Boosters
Propellant Handling Provisions at a Test Facility for Hypergolic Bipropellant Rocket Engines
Banc de tir pour moteur fusee a propergol solide a impact sonore reduit sur l'environnement
Establishing a Science-Based Environmental Cleanup Level for Liquid Propellant XM46
Possible Ways of Development of Ecologically Safe Solid Rocket Propellants
Recycling Military Energetic Materials into Products for Commercial Explosive Applications
A Complete Resource Recovery System for Solid Rocket Propellants
Prioritization Methodology for Chemical Replacement
Evaluation de l'impact sur l'environnement des essais statistiques de propulseur a propergol solide
Prevision du bruit impulsionnel des moteurs a tres court temps de combustion
Use of New Oxidizers and Binders to Meet Clean Air Requirements
Emission Spectroscopy and Pyrometry of Propellant Flames and Solid Rocket Exhaust Products
Environmental Impacts from Launching Chemical Rockets
Reclaimed and Virgin Ammonium Perchlorate Variations and How They Affect Solid Propellant Properties
Development of Environmentally Acceptable Propellants
Propergols solides pour lanceurs spatiaux generant pas ou peu de gaz chlorhydrique
The Impact of Space Rocket Launches on the Earth Ozone Layer
Development of Insensitive Rocket Propellants Based on Ammonium Nitrate and Polynimmo
Development of Less Polluting Propellants - Characteristic Features of AN/GAP Propellants
Biodegradation of Energetic Compounds: Application to Site Restoration
Improved Environmental Properties of a Solid Composite Propellant
Reduced Hazard Chemicals for Solid Rocket Motor Production
Shock Sensitivity of Ammonium Nitrate Propellants
Gas Pollutants From Ammonium Nitrate Based Propellants
Evaluation of Ammonium Nitrate Propellant Emissions
Destruction of Propellant Wastes Using Molten Salt Oxidation
Critical Fluid Demilitarization and Ingredient Reclamation Technology
Hydrazinium Nitroformate and Its Use as Oxidizer in High Performance Solid Propellants