Deterministic and Robust Optimization of Hybrid Rocket Engines for Small Satellite Launchers
Author:
Affiliation:
1. Politecnico di Torino, 10129 Torino, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35007
Reference28 articles.
1. Frequent and Reliable Launch for Small Satellites: Rocket Lab’s Electron Launch Vehicle and Photon Spacecraft
2. PLD Space’ Arion 2 micro-launcher; simplifying and improving the responsiveness in launch operations.
3. Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines
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