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Single Orbit Dynamics by Weiss%2c Benjamin%2c 1941
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1NASA Technical Reports Server (NTRS) 19820019475: Longitudinal Control Effectiveness And Entry Dynamics Of A Single-stage-to-orbit Vehicle
By NASA Technical Reports Server (NTRS)
The classical theory of flight dynamics for airplane longitudinal stability and control analysis was extended to the case of a hypervelocity reentry vehicle. This includes the elements inherent in supersonic and hypersonic flight such as the influence of the Mach number on aerodynamic characteristics, and the effect of the reaction control system and aerodynamic controls on the trim condition through a wide range of speed. Phugoid motion and angle of attack oscillation for typical cases of cruising flight, ballistic entry, and glide entry are investigated. In each case, closed form solutions for the variations in altitude, flight path angle, speed and angle of attack are obtained. The solutions explicitly display the influence of different regions design parameters and trajectory variables on the stability of the motion.
“NASA Technical Reports Server (NTRS) 19820019475: Longitudinal Control Effectiveness And Entry Dynamics Of A Single-stage-to-orbit Vehicle” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19820019475: Longitudinal Control Effectiveness And Entry Dynamics Of A Single-stage-to-orbit Vehicle
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19820019475: Longitudinal Control Effectiveness And Entry Dynamics Of A Single-stage-to-orbit Vehicle” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - AERODYNAMIC STABILITY - ATMOSPHERIC ENTRY - EULER EQUATIONS OF MOTION - LONGITUDINAL CONTROL - SINGLE STAGE TO ORBIT VEHICLES - SPACE TRANSPORTATION SYSTEM - ANGLE OF ATTACK - CONTROL CONFIGURED VEHICLES - OSCILLATIONS - OSCILLATORS - PITCH (INCLINATION) - REENTRY TRAJECTORIES - SPACECRAFT TRAJECTORIES - Vinh, N. X. - Lin, C. F.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19820019475
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 44.00 Mbs, the file-s for this book were downloaded 75 times, the file-s went public at Mon Aug 15 2016.
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2Spin-orbit Dynamics Of Single Acceptor Atoms In Silicon
By J. van der Heijden, T. Kobayashi, M. G. House, J. Salfi, S. Barraud, R. Lavieville, M. Y. Simmons and S. Rogge
Two-level quantum systems with strong spin-orbit coupling allow for all-electrical qubit control and long-distance qubit coupling via microwave and phonon cavities, making them of particular interest for scalable quantum information technologies. In silicon, a strong spin-orbit coupling exists within the spin-3/2 system of acceptor atoms and their energy levels and properties are expected to be highly tunable. Here we show the influence of local symmetry tuning on the acceptor spin-dynamics, measured in the single-atom regime. Spin-selective tunneling between two coupled boron atoms in a commercial CMOS transistor is utilised for spin-readout, which allows for the probing of the two-hole spin relaxation mechanisms. A relaxation-hotspot is measured and explained by the mixing of acceptor heavy and light hole states. Furthermore, excited state spectroscopy indicates a magnetic field controlled rotation of the quantization axes of the atoms. These observations demonstrate the tunability of the spin-orbit states and dynamics of this spin-3/2 system.
“Spin-orbit Dynamics Of Single Acceptor Atoms In Silicon” Metadata:
- Title: ➤ Spin-orbit Dynamics Of Single Acceptor Atoms In Silicon
- Authors: ➤ J. van der HeijdenT. KobayashiM. G. HouseJ. SalfiS. BarraudR. LavievilleM. Y. SimmonsS. Rogge
“Spin-orbit Dynamics Of Single Acceptor Atoms In Silicon” Subjects and Themes:
- Subjects: ➤ Mesoscale and Nanoscale Physics - Condensed Matter
Edition Identifiers:
- Internet Archive ID: arxiv-1703.03538
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 6.24 Mbs, the file-s for this book were downloaded 22 times, the file-s went public at Sat Jun 30 2018.
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3Single Orbit Dynamics
By Weiss, Benjamin, 1941-
Two-level quantum systems with strong spin-orbit coupling allow for all-electrical qubit control and long-distance qubit coupling via microwave and phonon cavities, making them of particular interest for scalable quantum information technologies. In silicon, a strong spin-orbit coupling exists within the spin-3/2 system of acceptor atoms and their energy levels and properties are expected to be highly tunable. Here we show the influence of local symmetry tuning on the acceptor spin-dynamics, measured in the single-atom regime. Spin-selective tunneling between two coupled boron atoms in a commercial CMOS transistor is utilised for spin-readout, which allows for the probing of the two-hole spin relaxation mechanisms. A relaxation-hotspot is measured and explained by the mixing of acceptor heavy and light hole states. Furthermore, excited state spectroscopy indicates a magnetic field controlled rotation of the quantization axes of the atoms. These observations demonstrate the tunability of the spin-orbit states and dynamics of this spin-3/2 system.
“Single Orbit Dynamics” Metadata:
- Title: Single Orbit Dynamics
- Author: Weiss, Benjamin, 1941-
- Language: English
“Single Orbit Dynamics” Subjects and Themes:
- Subjects: ➤ Ergodic theory -- Congresses - Orbit method -- Congresses - Stochastic processes -- Congresses
Edition Identifiers:
- Internet Archive ID: singleorbitdynam0000weis
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 338.91 Mbs, the file-s for this book were downloaded 52 times, the file-s went public at Fri Jan 07 2022.
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4NASA Technical Reports Server (NTRS) 19990062664: Inlet Development For A Rocket Based Combined Cycle, Single Stage To Orbit Vehicle Using Computational Fluid Dynamics
By NASA Technical Reports Server (NTRS)
Design and analysis of the inlet for a rocket based combined cycle engine is discussed. Computational fluid dynamics was used in both the design and subsequent analysis. Reynolds averaged Navier-Stokes simulations were performed using both perfect gas and real gas assumptions. An inlet design that operates over the required Mach number range from 0 to 12 was produced. Performance data for cycle analysis was post processed using a stream thrust averaging technique. A detailed performance database for cycle analysis is presented. The effect ot vehicle forebody compression on air capture is also examined.
“NASA Technical Reports Server (NTRS) 19990062664: Inlet Development For A Rocket Based Combined Cycle, Single Stage To Orbit Vehicle Using Computational Fluid Dynamics” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19990062664: Inlet Development For A Rocket Based Combined Cycle, Single Stage To Orbit Vehicle Using Computational Fluid Dynamics
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19990062664: Inlet Development For A Rocket Based Combined Cycle, Single Stage To Orbit Vehicle Using Computational Fluid Dynamics” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - INLET FLOW - DATA BASES - RELIABILITY ANALYSIS - REYNOLDS AVERAGING - SIMULATION - ORBITAL MANEUVERS - DESIGN ANALYSIS - COMPUTATIONAL FLUID DYNAMICS - CYCLES - IDEAL GAS - MACH NUMBER - REAL GASES - SINGLE STAGE TO ORBIT VEHICLES - DeBonis, J. R. - Trefny, C. J. - Steffen, C. J., Jr.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19990062664
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 17.28 Mbs, the file-s for this book were downloaded 73 times, the file-s went public at Sun Oct 16 2016.
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