Multi-disciplinary optimization of single-stage hybrid rockets for lunar ascent-Reference-Cited by-同舟云学术

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Multi-disciplinary optimization of single-stage hybrid rockets for lunar ascent

Published:2024-09 Issue: Volume:222 Page:493-507
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Zolla Paolo Maria^ORCID,Rosa Rodrigo,Migliorino Mario Tindaro,Bianchi Daniele^ORCID

Publisher

Elsevier BV

Reference56 articles.

1. Uncertainty analysis and design optimization of hybrid rocket motor powered vehicle for suborbital flight;Zhu;Chin. J. Aeronaut.,2015

2. On use of hybrid rocket propulsion for suborbital vehicles;Okninski;Acta Astronaut.,2018

3. Uncertainty analysis and robust design for a hybrid rocket upper stage;Casalino;J. Spacecr. Rockets,2019

4. Robust design approaches for hybrid rocket upper stage;Casalino;J. Aerosp. Eng.,2019

5. Hybrid rocket propulsion systems for outer planet exploration missions;Jens;Acta Astronaut.,2016

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