Tripropellant Engine Option Comparison for Single Stage to Orbit
Author:
Affiliation:
1. The Boeing Company, Canoga Park, California 91309-7922
2. NASA Marshall Space Flight Center, Huntsville, Alabama 35812
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3281
Reference19 articles.
1. Assessing single stage to orbit feasibility
2. The success of the X-33 depends on its technology—an overview
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1. Tripropellant Engine Technology for Reusable Launch Vehicles;Liquid Rocket Thrust Chambers;2004-01-01
2. Liquid Rocket Thrust Chambers;2004-01-01
3. Optimal performance of a tripropellant single-stage rocket;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24
4. Propellant Technologies: Far-Reaching Benefits for Aeronautical and Space-Vehicle Propulsion;Journal of Propulsion and Power;1998-09
5. Optimal Performance of a Dual-Fuel Single-Stage Rocket;Journal of Spacecraft and Rockets;1998-09
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