Download or read book Base flow Aerodynamics of a Saturn type Booster Stage at Mach Numbers 0 1 to 2 0 written by John L. Allen and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Base flow Aerodynamics of a Saturn type Booster Stage at Mach Numbers 0 1 to 2 0 written by John L. Allen and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1965 with total page 352 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1962 with total page 1116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1962 with total page 1472 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1962 with total page 962 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Aerodynamic Nozzle Hinge Moments of F 1 Engine Without Internal Flow on a Model of the S 1C Stage of Saturn 5 written by and published by . This book was released on 1965 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Exhaust Backflow from a Simulated Cluster of Three Wide spaced Rocket Nozzles in a Near space Environment written by James M. Cubbage and published by . This book was released on 1965 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: A limited experimental investigation has been conducted to confirm the existence of exhaust backflow from a cluster of three widely spaced nozzles operating in a near-space environment and to determine pressure and heat- transfer coefficients in the region washed by the backflow. Experiments were conducted in a 61-foot-diameter vacuum sphere using a sine solid-propellant rocket motor and a reflection plate. The reflection plate was used to simulate the interference planes that would normally exist for a cluster of three nozzles. Data were obtained for nozzle spacings of 8.02 and 17.05 nozzle exit diameters for pressures which simulated a nominal altitude range of 3.2 x 109(exp 5) to 1.8 x 10(exp 5) feet. The pressure data indicated that the backflow was super- sonic for several nozzle exit diameters ahead (upstream) of the nozzle exit plane and that the flow over small-diameter thermocouples in this region was in the free-molecule region. Average heat-transfer coefficients obtained for small-diameter cylinders (thermocouples) in this region were on the order of 1 x 10(exp -4) Btu/sq ft-sec-degrees R.
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:
Download or read book An Investigation of Base Heating on a 5 47 per cent Scale Model of the Saturn S 1 Booster at Transonic Mach Numbers written by T. L. Kennedy and published by . This book was released on 1961 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the 16-ft transonic tunnel of the propulsion wind tunnel facility at the Arnold Center to evaluate base heating of the Saturn S-1 booster. Various turbine exhaust stack configurations were tested over a Mach number range of 0.6 to 1.5, an altitude range of 10,000 ft to 42,000 ft, and a missile angle-of-attack range of 0 to -7 1/2 deg. Rocket engines using liquid oxygen and RP-1 were used to simulate the full-scale engine exhaust, and hydrogen was used to simulate the turbo-pump exhaust. Base burning at all test conditions was eliminated for only one of the turbine exhaust stack configurations. Various degrees of base burning were obtained for all other exhaust stack configurations, but no burning occurred at a free-stream Mach number of 1.5 for the trajectory altitude. At altitudes above 29,000 ft, only localized base burning occurred and the accompanying heating rates were low.
Download or read book Base Heat Transfer Pressure Ratios and Configuration Effects Obtained on a 1 27 Scall Saturn C 1 Model at Mach Numbers from 0 1 to 2 0 written by John L. Allen and published by . This book was released on 1963 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1963 with total page 748 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1975 with total page 970 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Download or read book Technical Publications Announcements with Indexes written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 1318 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Shadowgraph Study of the Upper Stage Flow Fields of Some Saturn V Study Configurations in the Transonic Mach Number Range written by C. Dale Andrews and published by . This book was released on 1965 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of Stage Separation Aerodynamics written by Robert A. Wasko and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at Mach Numbers from 0 60 to 1 20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster written by Albin O. Pearson and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
