Optimal Performance of a Dual-Fuel Single-Stage Rocket
Author:
Affiliation:
1. Turin Polytechnic Institute, Turin 10129, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3383
Reference12 articles.
1. Effects of tripropellant engines on earth-to-orbit vehicles
2. Dual-fuel propulsion in single-stage Advanced Manned Launch System Vehicle
3. Variable-mixture-ratio and other rocket engines for advanced shuttles
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