Explore: Ascent Trajectories
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Near-optimal operation of dual-fuel launch vehicles
By M. Ardema
“Near-optimal operation of dual-fuel launch vehicles” Metadata:
- Title: ➤ Near-optimal operation of dual-fuel launch vehicles
- Author: M. Ardema
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Reston, VA - [Washington, DC - Springfield, Va
“Near-optimal operation of dual-fuel launch vehicles” Subjects and Themes:
- Subjects: ➤ Guidance (Motion) - Single stage to orbit vehicles - Trajectory optimization - Propulsion system performance - Algorithms - Ascent trajectories - Mach number - Flight paths
Edition Identifiers:
- The Open Library ID: OL17837327M - OL17126502M - OL18121645M - OL15505687M
- Online Computer Library Center (OCLC) ID: 40217103
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
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2Optimal guidance law develpment for an advanced launch system
By Anthony J. Calise
“Optimal guidance law develpment for an advanced launch system” Metadata:
- Title: ➤ Optimal guidance law develpment for an advanced launch system
- Author: Anthony J. Calise
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Optimal guidance law develpment for an advanced launch system” Subjects and Themes:
- Subjects: ➤ Ascent trajectories - Launch vehicles - Trajectory optimization - Advanced launch system (STS) - Algorithms - Perturbation theory - Problem solving - Injection guidance - Real time operation - Spacecraft guidance - Transearth injection - Optimal control
Edition Identifiers:
- The Open Library ID: OL15416050M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Optimal guidance law develpment for an advanced launch system at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.