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Orbit insertion
Call for M5 Missions
Launch and Deployment Analysis for a Small, MEO, Technology Demonstration Satellite
Design of the Trajectory of a Tether Mission to Saturn
Utilizing Deep Reinforcement Learning to Effect Autonomous Orbit Transfers and Intercepts Via Electromagnetic Propulsion
VASIMR VX-200 Performance and Near-Term SEP Capability for Unmanned Mars Flight
Magnetoshell Aerocapture: Advances Toward Concept Feasibility
Space Sector Brochure
Astrox Studies and Experience with the Reusable Booster Systems and Two-Stage-To-Orbit Concepts
Aerocapture As an Enhancing Option for Ice Giants Missions
Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars by Larissa Balestrero Machado a Thesis S
+ Part 17: Acronyms and Abbreviations (265 Kb PDF)
Mercury Orbit Insertion March 18, 2011 UTC (March 17, 2011 EDT)
Launch and Deployment Analysis for a Small, MEO, Technology
Preparation of Papers for AIAA Technical Conferences
AAS 97-711 a Low-Cost Modified Launch Mode for High-C3
Assessment of Aerocapture-Entry Trajectories for Human Mars Exploration
Title: Lunar Orbit Cubesat Injector Primary Point of Contact (POC) & Email: J
Transfers to Lunar Libration Orbits
Top View
Trajectory Design Considerations for Exploration Mission 1
Revolutionizing Orbit Insertion with Active Magnetoshell Aerocapture
Aerocapture Project
A Dynamic Study of an Earth Orbiting Tether Propulsion System
Contingency Trajectory Design for a Lunar Orbit Insertion Maneuver Failure by the LADEE Spacecraft
Service Guide
Stationkeeping and Transfer Trajectory Design for Spacecraft in Cislunar Space Aas 17-826
Earth-Moon Near Rectilinear Halo and Butterfly Orbits for Lunar Surface Exploration
Performance Study of Two-Stage-To-Orbit Reusable Launch Vehicle Propulsion Alternatives
Electric Propulsion for Solar System Exploration
Part Iii : Space Transportation, Propulsion and Pathway Options
Lunar Orbit Insertion Targeting and Associated Outbound Mission Design for Lunar Sortie Missions
Air-Launch to Orbit
Juno Launch Press
Moon & Mars Orbiting Spinning Tether Transport (MMOSTT) (PDF
Electric Propulsion and Plasma Dynamics Laboratory
Applications of Tethers in Space
Section 2. Satellite Orbits
Firefly Aerospace OTV Payload User's Guide
Electrodynamic Tether Propulsion and Power Generation at Jupiter
Precision Orbit Control of the Advanced Land Observing Satellite (ALOS) for SAR Interferometry
Pegasus User Guide
ON MAKING USE of LUNAR and SOLAR GRAVITY ASSISTS in LUNAR-A, PLANET-B Missionst
VASIMR Rocket Design for a Mission to Mars [Pdf]
Reusability Analysis for Lunar Landers Ryan De Freitas Bart
Aerobraking Analysis for the Orbit Insertion Around Jupiter [Pdf]
Orbital Mechanics
4.2.1 Rockets and Launch Vehicles
Electric Propulsion for Geostationary Orbit Insertion
NASA In-Space Propulsion Systems Technology Area Roadmap
NASA Technology Roadmaps TA 2: In-Space Propulsion Technologies
• Advanced Propulsion for Geostationary Orbit Insertion and North-South Station Keeping
Hypersonic Airplane Space Tether Orbital Launch (Hastol) Architecture Study
Aerocapture Technology Developmnets by the In-Space
Advanced Electric Propulsion for RLV Launched Geosynchronous Spacecraft
Closed-Loop Endo-Atmospheric Ascent Guidance for Reusable Launch Vehicle Hongsheng Sun Iowa State University
Aas 11-509 Artemis Lunar Orbit Insertion and Science Orbit
Dare Mission Design: Low Rfi Observations from a Low-Altitude Frozen Lunar Orbit
Spacecraft Propulsion, Launch and Orbit Design Rocket Scientists Gift to Exoplanet Scientists
Aas 03-209 Messenger Mercury Orbit Trajectory
MESSENGER's Mercury Orbit Insertion Maneuver: Design
Aerocapture Design Study for a Titan Polar Orbiter
Chapter 3 General Performance Capabilities Table of Contents List of Figures
Increasing Space Access Availability for Small Payloads: the Pacastro
Transfers to Low Lunar Orbits
Space Debris Removal with Sub-Tethered Net: a Feasibility Study and Preliminary Design