Rendezvous and orbital docking
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Rendezvous and orbital docking a bibliography by Price, John F.

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Published by Space Technology Laboratories in Redondo Beach, Calif .
Written in English


  • Orbital rendezvous (Space flight) -- Bibliography.,
  • Orbital rendezvous (Space flight) -- Abstracts.

Book details:

Edition Notes

Statementby J. F. Price, and A. K. Dunlap.
SeriesSTL Technical Library. Advanced Research Group. Research bibliography ;, no. 47, Research bibliography (STL Technical Library. Advanced Research Group) ;, no. 47.
ContributionsDunlap, A. K., joint author.
LC ClassificationsZ5064.O7 P75
The Physical Object
Paginationiv, 138 p.
Number of Pages138
ID Numbers
Open LibraryOL5340419M
LC Control Number72194175

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Rendezvous requires a precise match of the orbital velocities of the two spacecraft, allowing them to remain at a constant distance through orbital station-keeping. Rendezvous may or may not be followed by docking or berthing, procedures which bring the spacecraft into physical contact and create a link between them. See also. It has been suggested that this page or section be merged with Tutorial: Orbital Rendezvous. In version docking was introduced. This allows two independently launched components to be intrinsically linked in orbit and allows them to function as a single structure. Functions of such a structure can range from a stationary way point, such as. Rendezvous during both orbital night nnd day - Use of only optical incasurcmcn& (no mdur) - Station-keeping and docking Simulbncouo countdown of dleser snd targct launch vehiclcs hunch during a narrow launch windou, Kcal Lime maneuver rsrge&~g using dam From pund bascd or onboard nzvigntion sensors Conduc~ing multiple rcndcmous operations in aFile Size: 1MB. Relative Motion in the Docking Phase of Orbital Rendezvous [Donald D Mueller] on *FREE* shipping on qualifying offers. Relative Motion in the Docking Phase of Author: Donald D Mueller.

Get this from a library! Automated rendezvous and docking of spacecraft. [Wigbert Fehse] -- This book is a reference for space engineers on all issues related to rendezvous and docking/berthing (RVD/B). It answers key questions such as: How does . Technology Development of Automated Rendezvous and efforts NASA has underway for Automated Rendezvous and Docking/Capture (AR&D/C) sensors and a docking mechanism and the challenges involved. The paper will additionally address Boeing’s Orbital Express was aFile Size: KB. To change your orbital plane by one degree requires a maneuver of over feet ( meters) per second. For the space shuttle, this would require nearly half of the shuttle’s entire on-orbit maneuvering capability, which must be also used for attitude control, orbital maneuvering, rendezvous and docking, separation, and deorbit.   Apollo 15 Rendezvous and Docking And when you have your Timeline Book out, I'd like to change some range and range-rate numbers because of this ellipticity of the Command Module orbit. Neither is the case here. The spacecraft are in somewhat different orbital planes, and the CSM's orbit is somewhat elliptical. To compensate for the out.

Rendezvous, Proximity, and Docking Orbital dynamics make rendezvous and proximity operations a complex task. Johnson Space Center (JSC) performs systems requirement definition, analyses, design, and testing necessary to support the development of rendezvous, proximity, and docking system designs and to verify theFile Size: KB.   Automated Rendezvous and Docking of Spacecraft - Ebook written by Wigbert Fehse. Read this book using Google Play Books app on your PC, android, iOS devices. Download for offline reading, highlight, bookmark or take notes while you read Automated Rendezvous and Docking of : Wigbert Fehse. The book provides an overview of the major issues governing approach and mating strategies, and system concepts for rendezvous and docking/berthing. These issues are described and explained such that aerospace engineers, students and even newcomers to the field can acquire a basic understanding of RVD/B. Sometimes they also do a R-bar rendezvous. In this case the secondary spacecraft approaches the primary along the local radial direction (X-direction in the RIC frame), but this requires many engine firings in the radial direction rather than only several altitude (and orbital velocity of the secondary) change manoeuvres.