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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
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Book Synopsis 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 by : George M. Yamakawa
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.
Book Synopsis 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 by : John I. Nagata
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.
Book Synopsis Technical Abstract Bulletin by : Defense Documentation Center (U.S.)
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:
Book Synopsis Engineering Flight Test of Uh-1b Helicopter Equipped with Xm-47 Antipersonnel Mine Dispensing Subsystem by : Manfred Reif
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.
Book Synopsis Engineering Flight Test of the Uh-1c Helicopter Equipped with the Xm-30 Weapon System by : Kenneth R. Ferrell
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.
Book Synopsis Flight Evaluation of the UH-1B Helicopter Equipped with an XM-5 Armament Kit by : Joseph M. Kudirka
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:
Book Synopsis 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 by : Jerry W. Petrie
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).
Book Synopsis Engineering Flight Test (product Improvement Test) of Production Oh-6a Helicopter Unarmed and Armed with the Xm-27e1 Weapon System Phase D by : John I. Nagata
Download or read book Engineering Flight Test (product Improvement Test) of Production Oh-6a Helicopter Unarmed and Armed with the Xm-27e1 Weapon System Phase D written by John I. Nagata and published by . This book was released on 1968 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: An engineering flight test of the OH-6A helicopter equipped with the XM-27E1 armament subsystem was conducted at Edwards Air Force Base, California, by the US Army Aviation Test Activity. The objective of the test was to determine what effects the armament subsystem had on the performance and stability and control characteristics as compared with an aircraft without the armament subsystem. The testing consisted of 10.25 productive test hours and was conducted from 2 October 1967 through 24 October 1967. Performance degradation resulted from the drag imposed by the armament subsystem. The specific range at 2400 pounds gross weight decreased by 8 percent. The stability and control characteristics were essentially unchanged by the addition of the armament subsystem. During firing tests, there were no adverse control problems. However, during flight at 12 degrees left sideslip at 105 knots indicated airspeed (KIAS), the upper right windshield imploded. The sideslip angle should be limited to 8 degrees or less at 100 KIAS until the cause of the implosion can be determined. Noise level and vibration tests should be conducted during firing with the 'doors off' configuration. The performance data should be incorporated into the operator's manual. (Author).
Book Synopsis Engineering Flight Test of the Ah-1g Helicopter Equipped with the Xm-20 Armament Subsystem (automatic 20mm Cannon). by : Stephen G. Dorris
Download or read book Engineering Flight Test of the Ah-1g Helicopter Equipped with the Xm-20 Armament Subsystem (automatic 20mm Cannon). written by Stephen G. Dorris and published by . This book was released on 1968 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: The engineering flight test of the AH-1G helicopter equipped with the XM-20 armament subsystem (automatic 20MM cannon) was conducted at Fort Hood, Texas from 31 January 1968 through 2 February 1968 by the US Army Aviation Test Activity, Edwards Air Force Base, California. Firing and nonfiring flight tests were conducted to determine the effects on the stability and control characteristics of the AH-1G helicopter caused by installation of the XM-20 armament subsystem. These tests were primarily qualitative in nature with limited qualitative data. The only stability and control characteristic which was affected either in the firing or nonfiring mode was the static longitudinal cyclic position gradients which were low at high speeds. The deficiencies detected during this test were the interference of the XM-20 gearbox with the XM-159 rocket pod and unreliability of the standard airspeed system due to the location of the static port in proximity to the XM-20 blast pressures. One firing rate of 600-800 spm is considered optimum. The XM-20 appears to offer greater stand-off capability, greater accuracy and more killing power than 2.75 inch rockets. It appears to be a reliable subsystem. The XM-20 configuration should be finalized, installed on a production AH-1G helicopter and certified for airworthiness throughout the AH-1G flight envelope as soon as possible to allow early introduction to Republic of Vietnam. (Author).
Book Synopsis Engineering Flight Test of the Uh-1b Helicopter Equipped with the Model 540 Rotor System. Phase D by : Laurel G. Schroers
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.
Book Synopsis Engineering Test of Uh-1b Helicopter Equipped with Floatation Landing Gear by : John T. Blaha
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.
Book Synopsis Engineering Flight Test: AH-1G (Hueycobra) Helicopter Equipped with the XM35 Armament Subsystem (20mm Automatic Gun) by : Gary C. Hall
Download or read book Engineering Flight Test: AH-1G (Hueycobra) Helicopter Equipped with the XM35 Armament Subsystem (20mm Automatic Gun) written by Gary C. Hall and published by . This book was released on 1969 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report of the Engineering Flight Test -- Performance Phase -- OH-5A Helicopter, Unarmed (Clean) and Armed with the XM-7 Or XM-8 Weapon Subsystem by :
Download or read book Report of the Engineering Flight Test -- Performance Phase -- OH-5A Helicopter, Unarmed (Clean) and Armed with the XM-7 Or XM-8 Weapon Subsystem written by and published by . This book was released on 1964 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt: Performance flight tests were conducted on the OH-5A helicopter to determine the compliance with the Light Observation Helicopter (LOH) Military Characteristics, to verify the contractual guarantees outlined in the OH-5A helicopter Model Specification and obtain additional data useful to the Selection Board.
Book Synopsis Report of the Engineering Flight Test -- Performance Phase -- of the OH-4A Helicopter, Unarmed (Clean) and Armed with the XM-7 Or XM-8 Weapon Subsystem by : ARMY AVIATION SYSTEMS TEST ACTIVITY EDWARDS AFB CA.
Download or read book Report of the Engineering Flight Test -- Performance Phase -- of the OH-4A Helicopter, Unarmed (Clean) and Armed with the XM-7 Or XM-8 Weapon Subsystem written by ARMY AVIATION SYSTEMS TEST ACTIVITY EDWARDS AFB CA. and published by . This book was released on 1964 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt: Performance flight tests were conducted on the OH-4A to determine the compliance with the Light Observation Helicopter (LOH) Military Characteristics and to Check the contractual guarantees outlined in the OH-4A Model Specification.
Book Synopsis Airworthiness and Flight Characteristics Test of the UH-60A Black Hawk Helicopter Equipped with the XM-139 Multiple Mine Dispensing System (VOLCANO) by :
Download or read book Airworthiness and Flight Characteristics Test of the UH-60A Black Hawk Helicopter Equipped with the XM-139 Multiple Mine Dispensing System (VOLCANO) written by and published by . This book was released on 1988 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Engineering Flight Test: AH-1G and UH-1H Helicopters Equipped with an Infrared Suppressor by : United States. Army Aviation Systems Test Activity
Download or read book Engineering Flight Test: AH-1G and UH-1H Helicopters Equipped with an Infrared Suppressor written by United States. Army Aviation Systems Test Activity and published by . This book was released on 1973 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Flight Test Data. Uh-1b High Performance Helicopter with Auxiliary Propulsion by : ARMY TRANSPORTATION RESEARCH COMMAND FORT EUSTIS VA.
Download or read book Preliminary Flight Test Data. Uh-1b High Performance Helicopter with Auxiliary Propulsion written by ARMY TRANSPORTATION RESEARCH COMMAND FORT EUSTIS VA. and published by . This book was released on 1964 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:
