Propellant mass fraction
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- C 2018 by Bindu Bhargavi Jagannatha. All Rights Reserved. SPACE LOGISTICS NETWORK OPTIMIZATION with EMBEDDED PROPULSION TECHNOLOGY SELECTION
- Optimization of Low-Thrust Gravity Assist Trajectories Under Application of Tisserand’S Criterion
- Earth-Mars Transfers with Ballistic Escape and Low-Thrust Capture G
- Rocket Performance
- Mars Ascent Vehicle (MAV) Solid Motor Technology Plans
- Arxiv:1805.03907V1 [Physics.Space-Ph] 10 May 2018
- Extension of Highly Elliptical Earth Orbits Using Continuous Low-Thrust Propulsion
- VISIONSPACE (ERC Project 227571)
- Technical Appendix
- Rho-Isp Revisited and Basic Stage Mass Estimating for Launch Vehicle Conceptual Sizing Studies
- Orbital Mechanics for Engineering Students to My Parents, Rondo and Geraldine, and My Wife, Connie Dee Orbital Mechanics for Engineering Students
- A Comparative Analysis of Single-Stage-To-Orbit Rocket and Air- Breathing Vehicles
- National Technical Information Service U.S
- Trajectory Design for Small-Satellite Missions to Near-Earth Objects Iaa-Lcpm-19-Xx-Xx
- Mission to Mars Vehicle Concept and Design
- Tsiolkovsky Rocket Equation from Wikipedia, the Free Encyclopedia
- Design and Optimization of Low-Thrust Gravity-Assist Trajectories to Selected Planets
- Low-Energy, Low-Thrust Transfers to the Moon