Investigation of Production Tolerances in Solid Propellant Tubular Grains
Gespeichert in:
Veröffentlicht in: | AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Solid rockets |
---|---|
1. Verfasser: | |
Weitere Verfasser: | , , |
Format: | UnknownFormat |
Sprache: | eng |
Veröffentlicht: |
2022
|
Schlagworte: | |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Titel | Jahr | Verfasser |
---|---|---|
Numerical Simulation of Multiphase Flows in Solid Rocket Motors Nozzles | 2022 | Grossi, Marco |
Effects of Vortex Flow Pancake Hybrid Rocket Engine Operating Parameters on Liquefying Fuel Combustion | 2022 | Hashish, Anwer |
Vega P80 SRM Pressure Oscillations Analysis by Means of Q1D Model | 2022 | Grossi, Marco |
Hypersonic Sounding Rocket System Design Optimization and Manufacturing | 2022 | Bolin, Robert E. |
Multiphysics Modelling for a Hybrid Rocket Engine with Liquefying Fuel: A Sensitivity Analysis on Combustion Instability | 2022 | Casalino, Lorenzo |
Low Temperature Solid Propellant Investigations for Mechanical Properties | 2022 | Barnhart, David |
Investigation of Production Tolerances in Solid Propellant Tubular Grains | 2022 | Adel, Hossam |
Ignition Characteristics of n-Butane/Oxygen-Enriched Air Mixture in Catalytic Micro-Channel | 2022 | Xin, Fang |