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Author : Joseph M. Kudirka
Publisher :
ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (898 download)
Download or read book Flight Evaluation of the UH-1B Helicopter Equipped with an XM-5 Armament Kit written by Joseph M. Kudirka and published by . This book was released on 1964 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : George M. Yamakawa
Publisher :
ISBN 13 :
Total Pages : 129 pages
Book Rating : 4.:/5 (227 download)
Download or read book Engineering Flight Test of Uh-1b Helicopter Equipped with Xm-16 Armament Subsystem and Engineering Flight Test of Uh-1b Helicopter Equipped with Xm-21 Armament Subsystem written by George M. Yamakawa and published by . This book was released on 1966 with total page 129 pages. Available in PDF, EPUB and Kindle. Book excerpt: Engineering flight tests of the UH-1B helicopter equipped with the XM-16 and XM-21 armament subsystems were conducted. The overall objective was to determine the effect of the installation of the subsystems on the UH-1B. Specific objectives were to determine the existence of any safety-of-flight conditions by evaluation of equantitative stability and control and vibration data and to determine any performance losses.
Author : John I. Nagata
Publisher :
ISBN 13 :
Total Pages : 135 pages
Book Rating : 4.:/5 (227 download)
Download or read book Engineering Flight Test of Uh-1b/540 Rotor Helicopter Equipped with Xm-16/m-5, Xm-21/m-5 Or Xm-3/m-5 Armament Subsystem written by John I. Nagata and published by . This book was released on 1966 with total page 135 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of an engineering flight test of the UH-1B/540 rotor helicopter equipped with the XM-16, XM-21, or XM-3 armament subsystem in conjunction with the M-5 armament subsystem. The test was conducted by the U.S. Army Aviation Test Activity (USAAVNTA). Overall test objectives were to verify safety of flight, develope data for the operator's manual, and assure that aircraft modifications did not degrade the handling qualities or limit the operational characteristics of the subsystems. Specific objectives were to determine quantitatively the effect of the armament subsystems on stability, control and performance of the aircraft, to determine the rocket launcher jettison characteristics, and to define the usable limits of the flight envelope for safe jettison of the launchers. Testing was conducted at Edwards Air Force Base, California, and at sites in Fort Irwin and Bakersfield, California. A total of 152 flights for a productive flight time of 116.4 hours was flown on aircraft S/N 64-14105 between 13 November 1965 and 5 May 1966. This included 30 jettison flights and 35 firing flights.
Author : Kenneth R. Ferrell
Publisher :
ISBN 13 :
Total Pages : 96 pages
Book Rating : 4.:/5 (227 download)
Download or read book Engineering Flight Test of the Uh-1c Helicopter Equipped with the Xm-30 Weapon System written by Kenneth R. Ferrell and published by . This book was released on 1967 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Army Preliminary Evaluation of the UH-1C/XM-30 weapon system was conducted by the U.S. Army Aviation Test Activity at Edwards Air Force Base and Fort Irwin, California. The degradation in level flight performance attributed to the weapon installation was defined and no objectionable flying qualities were encountered during firing or non-firing tests. The armed mission capability of the helicopter was degraded by high levels of stress, vibration, blast, and noise during firing and restrictive limitations were imposed by gun malfunctions and system gross weight. The reliability of the weapon system was poor and should be improved prior to further Army testing.
Author : Defense Documentation Center (U.S.)
Publisher :
ISBN 13 :
Total Pages : 784 pages
Book Rating : 4.:/5 (1 download)
Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. Superintendent of Documents
Publisher :
ISBN 13 :
Total Pages : 1248 pages
Book Rating : 4.:/5 (89 download)
Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1961 with total page 1248 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Edward I. Seto
Publisher :
ISBN 13 :
Total Pages : 107 pages
Book Rating : 4.:/5 (899 download)
Download or read book Flight Evaluation of the H-21C, HU-1A, and H-34C Equipped with XM-153 Armament Kit written by Edward I. Seto and published by . This book was released on 1962 with total page 107 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. Superintendent of Documents
Publisher :
ISBN 13 :
Total Pages : 1250 pages
Book Rating : 4.F/5 ( download)
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1979 with total page 1250 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 1958 pages
Book Rating : 4.3/5 (121 download)
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on with total page 1958 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jerry W. Petrie
Publisher :
ISBN 13 :
Total Pages : 95 pages
Book Rating : 4.:/5 (227 download)
Download or read book Engineering Flight Test of the Uh-1c Helicopter Equipped with the M-5 Grenade Launcher and the Xm-158 Or Xm-159 Airborne Rocket Launcher Pods Suspended from the Xm-156 Multiarmament Mount written by Jerry W. Petrie and published by . This book was released on 1967 with total page 95 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented are the results of engineering flight test of the UH-1C (UH-1B/540 rotor) helicopter equipped with the M-5 grenade launcher and the XM-158 or XM-159 airborne rocket launcher pods suspended from the X-156 multiarmament helicopter mount. Tests included 32 jettison flights for the XM-158 pods, 20 jettison flights for the XM-159 pods and 16 firings of the XM-159 pods. The objective was to determine quantitative effect of the XM-159 pods installed from the XM-156 mount on the stability, control and performance of the helicopter; to determine the XM-158 and XM-159 jettison characteristics and define the flight envelope for safe jettison of the pods; and to determine the flight envelope for firing the XM-159 pods. There were no significant adverse changes in the stability and control characteristics of the UH-1B/540 due to the installation of the XM-159. Previously reported longitudinal dynamic instability in climbs was also present throughout the tests. Self-excited undamped lateral 2/3-per-rev vibration was prevalent during the tests. Insufficient rocket-to-aircraft clearance for firing the XM-159 on the XM-156 mount was present without the addition of 4-inch cast aluminum spacers between the XM-156 mount and the universal pylon. The XM-159 was adjusted to maximum elevation to provide sufficient clearance for firing with the spacers installed. No major stability and control problems were encountered during the firing tests of the XM-159 or during the jettison tests of both the XM-158 and XM-159. Recommended flight envelopes were developed for jettison of both systems. (Author).
Author : John T. Blaha
Publisher :
ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.:/5 (227 download)
Download or read book Engineering Test of Uh-1b Helicopter Equipped with Floatation Landing Gear written by John T. Blaha and published by . This book was released on 1966 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: A limited engineering flight test evaluation of the UH-1B equipped with floatation landing gear was conducted by the U.S. Army Aviation Test Activity (USAAVNTA). The objectives of the program were to verify and amplify the data obtained during the manufacturer's flight testing and establish the basis for the Operator's Manual data to be used for UH-1B helicopters equipped with floatation landing gear. A total of 40 flights for 27 productive flight hours was flown at Edwards Air Force Base and Bakersfield, California, from 27 July 1965 through 10 September 1965. The UH-1B equipped with floatation landing gear could be flown with reasonable safety within a restricted flight envelope compared with a standard UH-1B. The water handling characteristics were considered excellent. Several warning statements and notations describing peculiarities in handling quantities were recommended for insertion in the Operator's Manual for operating UH-1B's with floatation landing gear. A restricted flight envelope was recommended for the UH-1B equipped with floatation landing gear. The performance test results were recommended for incorporation in the Operator's Manual.
Author : John T. Blaha
Publisher :
ISBN 13 :
Total Pages : 85 pages
Book Rating : 4.:/5 (899 download)
Download or read book Flight Test Evaluation of the HU-1B Helicopter Equipped with the 2.75 Aircraft Interim Area Rocket Weapon System written by John T. Blaha and published by . This book was released on 1963 with total page 85 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Manfred Reif
Publisher :
ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (227 download)
Download or read book Engineering Flight Test of Uh-1b Helicopter Equipped with Xm-47 Antipersonnel Mine Dispensing Subsystem written by Manfred Reif and published by . This book was released on 1966 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: A limited engineering flight test was conducted to provide sufficient engineering data for a safety-of-flight release for the UH-1B helicopter equipped with the XM-47 antipersonnel mine dispensing subsystem. An additional objective was to provide sufficient performance and stability and control data to update the operator's manual data to be used for UH-1B helicopters equipped with the XM-47 subsystem. Testing consisted of 42 productive flight hours. When the XM-47 mine dispensing subsystem was installed on the UH-1B helicopter, antipersonnel mines could be safely dispersed within the recommended flight envelopes. In cases of emergency the dispensers could be safely jettisoned within the recommended envelopes. Jettisons during entry into autorotation and in close proximity to the ground should be avoided. The flying qualities of the UH-1B were essentially unaffected by the installation of the XM-47 mine dispensing subsystem.
Author :
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.X/5 (1 download)
Download or read book Student Handbook written by and published by . This book was released on 1984 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Laurel G. Schroers
Publisher :
ISBN 13 :
Total Pages : 299 pages
Book Rating : 4.:/5 (227 download)
Download or read book Engineering Flight Test of the Uh-1b Helicopter Equipped with the Model 540 Rotor System. Phase D written by Laurel G. Schroers and published by . This book was released on 1966 with total page 299 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objectives of the test were to determine the airworthiness and to define the performance characteristics and flying qualities of the helicopter. Test Results, where appropriate, were compared with previous test results of the standard UH-1B. Tests were conducted at Edwards Air Force Base, California, and at remote test sites in California and Colorado from 19 May 1965 through 30 April 1966. Total aircraft flight time was 336.30 hours. Quantitative helicopter performance was defined for hovering, takeoff, climb, level flight, and autorotation. Stability and control characteristics were investigated for varied conditions of altitude, airspeed, center-of-gravity location, and gross weight.
Author : Robert J. Reschak
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (898 download)
Download or read book UH-1B/AN/ASW-12ıVı Flight Evaluation of the Production Configuration./ Robert J. Reschak and Gene L. Colvin written by Robert J. Reschak and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Daniel W. Lester
Publisher :
ISBN 13 :
Total Pages : 544 pages
Book Rating : 4.:/5 (321 download)
Download or read book Cumulative Title Index to United States Public Documents, 1789-1976 written by Daniel W. Lester and published by . This book was released on 1980 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:
