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Aerodynamic Abort Separation Characteristics Of A Parallel Staged Reusable Launch Vehicle From Mach 060 To 120
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Book Synopsis Aerodynamic Abort-separation Characteristics of a Parallel-staged Reusable Launch Vehicle from Mach 0.60 to 1.20 by :
Download or read book Aerodynamic Abort-separation Characteristics of a Parallel-staged Reusable Launch Vehicle from Mach 0.60 to 1.20 written by and published by . This book was released on 1965 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Separation Characteristics of Conceptual Parallel-staged Reusable Launch Vehicle at Mach 3 to Mach 6 by :
Download or read book Aerodynamic Separation Characteristics of Conceptual Parallel-staged Reusable Launch Vehicle at Mach 3 to Mach 6 written by and published by . This book was released on 1965 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Lateral Aerodynamic Characteristics of a Conceptual Horizontal-take-off Reusable Launch Vehicle from Mach 3 to 6 by :
Download or read book Lateral Aerodynamic Characteristics of a Conceptual Horizontal-take-off Reusable Launch Vehicle from Mach 3 to 6 written by and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 by :
Download or read book Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of a Model of a Horizontal Take Off Reusable Launch Vehicle at Mach Numbers from 3 to 6 by :
Download or read book Longitudinal Aerodynamic Characteristics of a Model of a Horizontal Take Off Reusable Launch Vehicle at Mach Numbers from 3 to 6 written by and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Interference Effects Caused by Parallel-staged Simple Aerodynamic Configurations at Mach Numbers of 3 and 6 by : John P. Decker
Download or read book Aerodynamic Interference Effects Caused by Parallel-staged Simple Aerodynamic Configurations at Mach Numbers of 3 and 6 written by John P. Decker and published by . This book was released on 1969 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach numbers of 3 and 6.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1972 with total page 1056 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach 2.96 and 4.61 of a Reusable Launch Vehicle Based on Supersonic Transport Airplane Design by :
Download or read book Aerodynamic Characteristics at Mach 2.96 and 4.61 of a Reusable Launch Vehicle Based on Supersonic Transport Airplane Design written by and published by . This book was released on 1966 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Complete VTO Launch Vehicle and Reusable Flyback Configuration from Mach 3.0 to 6.0 by :
Download or read book Aerodynamic Characteristics of a Complete VTO Launch Vehicle and Reusable Flyback Configuration from Mach 3.0 to 6.0 written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Loading Characteristics of a 1/10-scale Model of the Three-stage Scout Vehicle at Mach Numbers 1.57 to 4.65 by : Lloyd S. Jernell
Download or read book Aerodynamic Loading Characteristics of a 1/10-scale Model of the Three-stage Scout Vehicle at Mach Numbers 1.57 to 4.65 written by Lloyd S. Jernell and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Optimal Control Theory Determination of Feasible Return-to-launch-site Aborts for the HL-20 Personnel Launch System Vehicle by : Kevin E. Dutton
Download or read book Optimal Control Theory Determination of Feasible Return-to-launch-site Aborts for the HL-20 Personnel Launch System Vehicle written by Kevin E. Dutton and published by . This book was released on 1994 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Loading Characteristics at Mach Numbers from 0.80 to 1.20 of a 1/10-scale Three-stage Scout Model by : Thomas C. Kelly
Download or read book Aerodynamic Loading Characteristics at Mach Numbers from 0.80 to 1.20 of a 1/10-scale Three-stage Scout Model written by Thomas C. Kelly and published by . This book was released on 1961 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic loads results have been obtained in the Langley 8-foot transonic pressure tunnel at Mach numbers from 0.80 to 1.20 for a 1/10-scale model of the upper three stages of the Scout vehicle. Tests were conducted through an angle-of-attack range from -8° to 8° at an average test Reynolds number per foot of about 4.0 x 106. Results indicated that the peak negative pressures associated with expansion corners at the nose and transition flare exhibit sizeable variations which occur over a relatively small Mach number range. The magnitude of the variations may cause the critical local loading condition for the full-scale vehicle to occur at a Mach number considerably lower than that at which the maximum dynamic pressure occurs in flight. The addition of protuberances simulating antennas and wiring conduits had slight, localized effects. The lift carryover from the nose and transition flare on the cylindrical portions of the model generally increased with an increase in Mach number.
Book Synopsis Longitudinal Control and Footprint Analysis for a Reusable Military Launch Vehicle by : Anhtuan D. Ngo
Download or read book Longitudinal Control and Footprint Analysis for a Reusable Military Launch Vehicle written by Anhtuan D. Ngo and published by . This book was released on 2003 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this paper, we will examine a configuration for a reusable military launch vehicle (RMLS) concept. This configuration allows for the vehicle to land in an inverted attitude. Such inverted landing improves the turnaround time of the vehicle by reducing the maintenance requirements of the vehicle's thermal protection system. An analysis is performed to examine the impacts by the configuration on stability, control, and footprint for an RMLS configuration.
Book Synopsis Effects of Configuration Geometry on the Transonic Aerodynamic Characteristics of a Simulated Launch Vehicle by :
Download or read book Effects of Configuration Geometry on the Transonic Aerodynamic Characteristics of a Simulated Launch Vehicle written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Footprint Determination for Reusable Launch Vehicles Experiencing Control Effector Failures by : David B. Doman
Download or read book Footprint Determination for Reusable Launch Vehicles Experiencing Control Effector Failures written by David B. Doman and published by . This book was released on 2002 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt: The ability to compute the maximum area on the earth's surface (footprint) reachable by an autonomous air vehicle can be useful in planning for the vehicle's safe operations. The information can be important when the vehicle experiences subsystem failures causing it to be unable to maintain its nominal performance. In this paper, we present a method to calculate the footprint of a reusable launch vehicle that experiences a failure in one or more of its aero-control surfaces. During a control effector failure, the maximum attainable moments of the vehicle are reduced, which may decrease the range of conditions that the vehicle can maintain a trimmed condition. Additionally, the lift and drag characteristics of the vehicle can change when control effectors are moved to off-nominal positions to correct for moment imbalance caused by failures or damage. As a result, the footprint of the vehicle is reduced. A technique for calculating the available effectiveness of the aero-control surfaces is used in conjunction with a footprint generation algorithm to include the effects of rotational trim on the vehicle footprint.
Book Synopsis Launch Vehicle Design Process: Characterization, Technical Integration, and Lessons Learned by : J. C. Blair
Download or read book Launch Vehicle Design Process: Characterization, Technical Integration, and Lessons Learned written by J. C. Blair and published by . This book was released on 2001 with total page 264 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 0.10-scale Model of a Three-stage Configuration of the Scout Research Vehicle at Mach Numbers of 2.29, 2.96, 3.96, and 4.65 by : Lloyd S. Jernell
Download or read book Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 0.10-scale Model of a Three-stage Configuration of the Scout Research Vehicle at Mach Numbers of 2.29, 2.96, 3.96, and 4.65 written by Lloyd S. Jernell and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
