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The purpose of this research was to parametrically investigate the viability of skip entry maneuvers as an alternative to vacuum-only maneuvers, and to identify whether skip entry maneuvers can extend spacecraft mission lifetime by limiting propellant expenditure through the exploitation of the aerodynamic interaction between the upper atmosphere and an example entry vehicle and remote-sensing orbital platform. Employing the X-37B Orbital Test Vehicle (OTV) and a notional satellite design as the example entry vehicles, the entry profile dynamics of a skip entry maneuver were characterized with varying trajectory initial conditions such as entry altitude, entry flight-path angle, and vehicle aerodynamics. In addition, the ?? requirements of skip entry maneuvers were characterized, specifically the ?? required to complete one or more successive skip entry trajectories as well as to execute a desired change in orbit inclination angle.
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The purpose of this research was to parametrically investigate the viability of skip entry maneuvers as an alternative to vacuum-only maneuvers, and to identify whether skip entry maneuvers can extend spacecraft mission lifetime by limiting propellant expenditure through the exploitation of the aerodynamic interaction between the upper atmosphere and an example entry vehicle and remote-sensing orbital platform. Employing the X-37B Orbital Test Vehicle (OTV) and a notional satellite design as the example entry vehicles, the entry profile dynamics of a skip entry maneuver were characterized with varying trajectory initial conditions such as entry altitude, entry flight-path angle, and vehicle aerodynamics. In addition, the ?? requirements of skip entry maneuvers were characterized, specifically the ?? required to complete one or more successive skip entry trajectories as well as to execute a desired change in orbit inclination angle.
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- VerlagBiblioScholar
- Erscheinungsdatum2012
- ISBN 10 1249831091
- ISBN 13 9781249831099
- EinbandTapa blanda
- SpracheEnglisch
- Anzahl der Seiten168
- Kontakt zum HerstellerNicht verfügbar
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Spacecraft Demand Tasking and Skip Entry Responsive Maneuvers
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Zustand: New. KlappentextrnrnThe purpose of this research was to parametrically investigate the viability of skip entry maneuvers as an alternative to vacuum-only maneuvers, and to identify whether skip entry maneuvers can extend spacecraft mission lifetime b. Artikel-Nr. 6488984
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Spacecraft Demand Tasking and Skip Entry Responsive Maneuvers
Verlag:
Creative Media Partners, LLC Okt 2012, 2012
ISBN 10: 1249831091
ISBN 13: 9781249831099
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Taschenbuch. Zustand: Neu. Neuware - The purpose of this research was to parametrically investigate the viability of skip entry maneuvers as an alternative to vacuum-only maneuvers, and to identify whether skip entry maneuvers can extend spacecraft mission lifetime by limiting propellant expenditure through the exploitation of the aerodynamic interaction between the upper atmosphere and an example entry vehicle and remote-sensing orbital platform. Employing the X-37B Orbital Test Vehicle (OTV) and a notional satellite design as the example entry vehicles, the entry profile dynamics of a skip entry maneuver were characterized with varying trajectory initial conditions such as entry altitude, entry flight-path angle, and vehicle aerodynamics. In addition, the requirements of skip entry maneuvers were characterized, specifically the required to complete one or more successive skip entry trajectories as well as to execute a desired change in orbit inclination angle. Artikel-Nr. 9781249831099
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