Download or read book The Static Stability Characteristics of Several Configurations of the Aft entry Ducted ram rocket Rv n i at Subsonic and Supersonic Speeds written by WALLACE. LUCHUK and published by . This book was released on 1957 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Stability and Separation Characteristics of a Two stage Rocket Configuration at Mach Numbers from 1 57 to 4 50 written by Kenneth L. Turner and published by . This book was released on 1960 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of a Rocket Vehicle with Thick Wedge Fins and Sweptback Leading and Trailing Edges written by Joseph A. Yuska and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The longitudinal static stability characteristics of three one-fifth scale models of the second stage of a sounding rocket were calculated and compared with the measured values at Mach numbers of 1.79 to 3.47. All three models had fins of trapezoidal planform with sweptback leading and trailing edges, small aspect ratio, and thick wedge sections, but differed in fin area and overall model length. Calculation of center of pressure and normal-force coefficient slope at zero normal force were in good agreement with experimental data.
Download or read book Static Stability and Magnus Characteristics of the 5 inch High Capacity Spinner Rocket at Low Subsonic Speeds written by J. E. Greene and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: The static stability and Magnus characteristics of a 1.227 scale model of the 5-inch High Capacity Spinner Rocket have been determined for yaw angles of 0 degree through 28 degrees and for spin rates up to 10,000 RPM. The maximum diameter of the model was 6 inches. These tests were performed in the DTMB 8 x 10 foot low subsonic wind tunnel at speeds of 211 and 260 feet per second. The results of this investigation show that the Magnus force and moment characteristics of the projectile are non-linear functions of the body spin rate and angle of yaw. In addition, the test results also show that high rotational speeds make the configuration less unstable, statically, and my, under certain conditions of spin and yaw, cause the rocket to be statically stable.
Download or read book Static Aerodynamic Characteristics of a Three stage Rocket Vehicle Having Various Fin Configurations at Low Subsonic Mach Numbers and Angles of Attack Up to 28 written by Clarence A. Brown and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Stability and Magnus Characteristics of the 5 caliber and 7 caliber Army navy Spinner Rocket at Low Subsonic Speeds written by J. E. GREEN and published by . This book was released on 1954 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low subsonic speed Static Stability of Right triangular pyramid and Half cone Lifting Reentry Configurations written by George M. Ware and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract:
Download or read book Static Aerodynamic Characteristics of Three Rocket vehicle Configurations at Mach Numbers from 1 80 to 4 63 Including Some Effects of Fin Size Fin Cant and Auxiliary Rocket Motors written by Dennis E. Fuller and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low subsonic speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry vehicle Configuration Having Wingtip Panels that Fold Up for High drag Reentry written by George M. Ware and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of a Two stage and a Three stage Rocket Vehicle at Mach Numbers from 1 47 to 4 63 written by Clarence A. Brown and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of a Three stage Rocket Vehicle Having Various Fin Configurations at Low Subsonic Mach Numbers and Angles of Attack Up to 28 Degrees written by Clarence A. Jr Brown and published by . This book was released on 1963 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Engineering the Space Age a Rocket Scientist Remembers written by Robert Brulle and published by Createspace Independent Publishing Platform. This book was released on 2012-08 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Rarely is a reader exposed to such an extraordinary, multifaceted presentation of aerospace technology as Bob Brulle narrates in this book. After returning from duty as a combat fighter pilot in World War II, this Belgian immigrant developed a multitalented and innovative aerospace career path that addressed many of the aerospace professions. Along the way he forged a career in the aviation and space field that resulted in his participating in several of the most momentous aerospace achievements of the past century. He also expanded his education through hard work to a level at which he was qualified to teach graduate-level aerospace engineering courses. It is interesting to follow how the analysis and design techniques of aerospace vehicles progressed over the years, which incidentally reveals the large role that the computer played in making that possible. The story on the early Cape Canaveral operations was amusing and showed that enterprising innovations played a large role in a successful undertaking. Some of the projects described were a surprise, as I had never heard of them, like reading how a pencil-shaped missile was built that could fly and maneuver over an intercontinental distance at a high hypersonic velocity. He also described how American engineers and scientists fought the Cold War battle for technological supremacy on their desks and in their laboratories. The initiatives by which this enterprising engineer develops his technical approach to a project are very informative and offer the reader an insight into the workings of successful operations. He achieves an interesting behind-the-scenes look at how aerospace history is made by weaving in the historical significance of these projects as they are developed. As a former aeronautical engineer at the rapidly growing Mc- Donnell Aircraft Corporation, Bob gives us an interesting exposure to the importance of top management's relationship with the workforce in a successful company. "Mr. Mac" made it a point to make all his employees team members by frequent communication and friendly association.
Download or read book Wind tunnel Investigation at High Subsonic Speeds to Determine Stability and Control Characteristics of Antitank Missiles with Ram pressure Jet Controls on a Ring Tail written by Raymond D. Vogler and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of Three Rocket vehicle Configurations at Mach Numbers from 1 80 to 4 63 Including Some Effects of Fin Size Fin Cant and Auxiliary Rocket Motors written by Dennis E. Fuller and published by . This book was released on 1963 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Static Stability Characteristics of Two Configurations Suitable for Lifting Reentry from Satellite Orbit written by John W. Paulson and published by . This book was released on 1958 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Controls written by William A. Corlett and published by . This book was released on 1979 with total page 117 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted to determine the static stability and control characteristics of a cruciform missile configuration with delta wings and aft tail fin controls. The tests were conducted in the Langley Unitary Plan wind tunnel at Mach numbers from 1.60 to 4.63 through an angle-of-attack range of -4 degree to 30 degree. Model roll orientation was varied from 0 degree to 135 degree. The results indicated good longitudinal stability and control characteristics throughout the test Mach number range. Relatively high induced rolling and yawing moments were apparent at asymmetric model roll angles for the lower test Mach numbers; however, sufficient roll and yaw control was available to trim to relatively high angles of attack and lift coefficients. (Author).
Download or read book Static Aerodynamic Characteristics of a Two stage and a Three stage Rocket Vehicle at Mach Numbers from 1 47 to 4 63 written by CLARENCE A. JR. BROWN and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley Unitary Plan wind tunnel to determine the effects of fin cant and size on the static aerodynamic characteristics of a 0.081-scale model of a three-stage and a two-stage Trailblazer II configuration. Tests were performed at Mach numbers from 1.47 to 4.63 and at a Reynolds number per foot of 3.0 x 10 to the 6th power. he angleof-attack range varied from approximately -5 to 5 degrees and angle of sideslip varied from approximately -4 to 4 degrees. All first-stage fins tested gave adequate static stability when the center-of-gravity travel of the flight model was taken into account. The presence of the auxiliary rocket motors in the lateral plane decreased the effectiveness of the fins in the pitch plane at the lower Mach number and increased the fin effectiveness at the higher Mach numbers. Removal of the auxiliary rocket motors from the first stage of the two-stage configuration reduced the axial force about 25% at the low Mach numbers and about 15% at the high Mach numbers. (Author).
