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Static Stability And Pressure Test Of A 004 Scale Model Of The Apollo Saturn V Vehicle At Mach Numbers From 060 Through 140
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Book Synopsis STATIC STABILITY AND PRESSURE TEST OF A 0.04-SCALE MODEL OF THE APOLLO SATURN V VEHICLE AT MACH NUMBERS FROM 0.60 THROUGH 1.40 by :
Download or read book STATIC STABILITY AND PRESSURE TEST OF A 0.04-SCALE MODEL OF THE APOLLO SATURN V VEHICLE AT MACH NUMBERS FROM 0.60 THROUGH 1.40 written by and published by . This book was released on 1968 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: A 0.04-scale model of the Saturn V Missile was tested at transonic Mach numbers to determine Reynolds number effects on static stability characteristics and pressure distributions in the tail barrel region at high angles of attack. Reynolds number based on the model diameter varied from 0.9 to 8.4 million. Angle of attack was varied from -3 to 16 deg. The center of pressure varied with angle of attack over a distance of approximately one model diameter.
Book Synopsis PRESSURE TEST ON A 0.04-SCALE MODEL OF THE SATURN V LAUNCH VEHICLE AT MACH NUMBERS FROM 0.60 THROUGH 1.45 by :
Download or read book PRESSURE TEST ON A 0.04-SCALE MODEL OF THE SATURN V LAUNCH VEHICLE AT MACH NUMBERS FROM 0.60 THROUGH 1.45 written by and published by . This book was released on 1966 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static pressure distribution and boundary-layer profiles were obtained on a 0.04-scale model of the Saturn V vehicle at Mach numbers from 0.60 to 1.45. The Reynolds number based on the model diameter varied from 3.3 to 6.0 million. Unsteady pressures were also measured over the full Mach number range; however, these data are not presented in this report. Protuberances on the model affected local static pressures, but did not alter the overall distribution significantly.
Book Synopsis PRESSURE TEST ON A 0.04-SCALE MODEL OF THE SATURN V LAUNCH VEHICLE AT MACH NUMBERS FROM 1.80 THROUGH 3.00 by :
Download or read book PRESSURE TEST ON A 0.04-SCALE MODEL OF THE SATURN V LAUNCH VEHICLE AT MACH NUMBERS FROM 1.80 THROUGH 3.00 written by and published by . This book was released on 1967 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt: In conjunction with an earlier transonic test, a 0.04-scale model of the Saturn V launch vehicle was tested at Mach numbers from 1.80 to 3.00 for Reynolds number based on model diameter varying from 1.59 to 2.77 million. Static pressure distributions and boundary-layer profiles were measured and are presented herein.
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 850 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Signatures for a .00053 Scale Model of the Saturn 5-Apollo Launch Vehicle with Simulated Exhaust Plumes by :
Download or read book Pressure Signatures for a .00053 Scale Model of the Saturn 5-Apollo Launch Vehicle with Simulated Exhaust Plumes written by and published by . This book was released on 1973 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Control Characteristics of a 0.030-scale Model of a Little Joe 2-Apollo Space Vehicle at Mach Numbers from 1.57 to 4.65 by :
Download or read book Static Stability and Control Characteristics of a 0.030-scale Model of a Little Joe 2-Apollo Space Vehicle at Mach Numbers from 1.57 to 4.65 written by and published by . This book was released on 1963 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 by : Dennis E. Fuller
Download or read book Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 written by Dennis E. Fuller and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 by : Dennis E. Fuller
Download or read book Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 written by Dennis E. Fuller and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of a Model of a Two-stage Version of a Saturn Launch Vehicle with a Proposed Apollo Payload at Mach Numbers from 1.57 to 2.87 by :
Download or read book Static Longitudinal Aerodynamic Characteristics of a Model of a Two-stage Version of a Saturn Launch Vehicle with a Proposed Apollo Payload at Mach Numbers from 1.57 to 2.87 written by and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Model of a Saturn 1 Block 2 Launch Vehicle with Proposed Spacecraft at Mach Numbers from 1.57 to 2.87 by :
Download or read book Static Aerodynamic Characteristics of a Model of a Saturn 1 Block 2 Launch Vehicle with Proposed Spacecraft at Mach Numbers from 1.57 to 2.87 written by and published by . This book was released on 1964 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis FORCE TESTS OF THE SATURN V LOR AND SATURN 1B/AS-206 CONFIGURATIONS AT MACH NUMBERS 1.5 THROUGH 8 by :
Download or read book FORCE TESTS OF THE SATURN V LOR AND SATURN 1B/AS-206 CONFIGURATIONS AT MACH NUMBERS 1.5 THROUGH 8 written by and published by . This book was released on 1967 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static force tests were conducted on models of the Saturn V LOR and Saturn 1B/AS-206. Data were obtained at Mach numbers 1.5 through 8 at angles of attack from -4 to 13 deg. The Reynolds number, based on the booster diameter, ranged from 24,000 to 1,670,000. The results presented show the effects of Mach number and model attitude on the static longitudinal stability and axial-force characteristics.
Book Synopsis Static Longitudinal Aerodynamic Characteristics of a 0.028-scale Model of a Proposed Little Joe-Apollo Space Vehicle at Mach Numbers from 0.50 to 1.20 by :
Download or read book Static Longitudinal Aerodynamic Characteristics of a 0.028-scale Model of a Proposed Little Joe-Apollo Space Vehicle at Mach Numbers from 0.50 to 1.20 written by and published by . This book was released on 1962 with total page 20 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:
Book Synopsis Measurements of the Mach Number and Pressure on the Afterbody of a Blunt-nosed Model in Free Flight at Mach Numbers from 6.5 to 14 by : Simon C. Sommer
Download or read book Measurements of the Mach Number and Pressure on the Afterbody of a Blunt-nosed Model in Free Flight at Mach Numbers from 6.5 to 14 written by Simon C. Sommer and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Signatures for the Apollo Command Module and the Saturn 5 Launch Vehicle with a Discussion of Strong Shock Extrapolation Procedures by :
Download or read book Pressure Signatures for the Apollo Command Module and the Saturn 5 Launch Vehicle with a Discussion of Strong Shock Extrapolation Procedures written by and published by . This book was released on 1972 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government reports annual index by :
Download or read book Government reports annual index written by and published by . This book was released on 199? with total page 1048 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Stability Characteristics of the Apollo Launch Escape Vehicle by : William C. Moseley (Jr.)
Download or read book Aerodynamic Stability Characteristics of the Apollo Launch Escape Vehicle written by William C. Moseley (Jr.) and published by . This book was released on 1967 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
