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Mass ratio
Rocket Equation
Rocket Basics 1: Thrust and Specific Impulse
MARYLAND Orbital Mechanics
The Effects of Barycentric and Asymmetric Transverse Velocities on Eclipse and Transit Times
A Conceptual Analysis of Spacecraft Air Launch Methods
N-Body Dynamics of Intermediate Mass-Ratio Inspirals in Star Clusters Haster, Carl-Johan; Antonini, Fabio; Kalogera, Vicky; Mandel, Ilya
Revolutionary Propulsion Concepts for Small Satellites
Debris Assessment Software User’S Guide
RWTH Aachen University Institute of Jet Propulsion and Turbomachinery
Lecture 7 Launch Trajectories
A New Radial Velocity Curve, Apsidal Motion, and the Alignment of Rotation and Orbit Axes
AIAA 2001-3377 Solar Thermal Propulsion for an Interstellar Probe
Optimization of Low-Thrust Gravity Assist Trajectories Under Application of Tisserand’S Criterion
Spin–Orbit Precession for Eccentric Black Hole Binaries at First Order in the Mass Ratio
A Historical Review of the Theory of Gravity-Assists in the Pre-Spaceflight
Mass Ratios of Long-Period Binary Stars Resolved in Precision Astrometry Catalogs of Two Epochs
A REACTION DRIVE Powered by External Dynamic Pressure
Rocket Performance
Top View
Capability of Solar Electric Propulsion for Planetary Missions Giuseppe D
LOS ALAMOS SCIENTIFIC LABORATORY of the UNIVERSITYOF Californiao LOSALAMOS NEW MEXICO
THE RESTRICTED P + 2 BODY Problemt
California State Science Fair
An Air-Breathing Launch Vehicle Concept for Single-Stage-To-Orbit
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
Combining Solar Sails with the Oberth Effect
Arxiv:2107.02700V2 [Gr-Qc] 7 Jul 2021
Gravity-Assist Maneuvers Augmented by the Lorentz Force
Appendix a Equations and Supporting Data
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Rocket Performance
ORBITAL TRANSFERS: OPTIMIZATION METHODS and RECENT RESULTS Mauro Pontani 1. Introduction. on January 2, 1959, the Soviet Luna 2
Exomoons” from Photometric Transit Timing Variations (Research Note)
Design and Development of Single-St Age-To-Orbit Vehicles
Gravitational Assisted Trajectories Lectures E
Arxiv:1803.04833V1 [Astro-Ph.SR] 13 Mar 2018 Esug 954Russia 198504 Tersburg, Russia 196140 Petersburg, .Ptrbr Tt Nvriy ..Sblvatooia Ins Astronomical Sobolev V.V
A Solution to the Circular Restricted N Body Problem in Planetary Systems
October 2017 Presentation
Basics Chemical Rocket Thrust Specific Impulse Rocket Equation
Smart Propellant
Adiabatic Waveforms for Extreme Mass-Ratio Inspirals Via Multivoice Decomposition in Time and Frequency
A Single-Stage Reusable Launch Vehicle Concept Abbos Yunusov A