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Propellant mass fraction
Electric Propulsion System Scaling for Asteroid Capture-And-Return Missions
Orbital Fueling Architectures Leveraging Commercial Launch Vehicles for More Affordable Human Exploration
Conceptual Design and Optimization of Hybrid Rockets
Performance Modelling and Simulation of a 100 Km Hybrid Sounding Rocket
19760011102.Pdf
Preliminary Design of Nuclear Electric Propulsion Missions to the Outer Planets
Spiral Trajectories in Global Optimisation of Interplanetary and Orbital Transfers Final Report
UC3M Analysis of Orbital Relay Stations for Orbital Energy
Acta Futura 11 (2018) 25-35 Acta DOI: 10.5281/Zenodo.1139152 Futura
Preparation of Papers for AIAA Technical Conferences
A Conceptual Analysis of Spacecraft Air Launch Methods
Arxiv:1206.1336V2 [Math.OC] 29 Jun 2012 Omnms H Oa Asi Pc N Aiietedflcino H a Obt the Be of Keywords: Can Deflection Spacecraft
The Motion of a Rocket
Revolutionary Propulsion Concepts for Small Satellites
A Generic Mission Architecture Sizing Tool
A Di Ingegneria Low Thrust Trajectories in Multi Body
RWTH Aachen University Institute of Jet Propulsion and Turbomachinery
Propulsion System
Top View
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
Time-Optimal Trajectories to Circumsolar Space Using Solar
C:\SAVE ME\Aoe2104\8Spaceflight.Wpd
Optimization of Reconfigurable Satellite Constellations Using
NASA Lunar Lander Reference Design (2019)
Optimization and Design for Heavy Lift Launch Vehicles
Rapid Mars Transits with Exhaust- Modulated Plasma Propulsion
A Novel Method for Low-Thrust Gravity-Assist Trajectory Optimization
Smart Propellant