Specification for F-106A/B Aircraft Weapon Control Systems; (Type MA-1 and ASQ-25) Production Alignment and Test Procedures Report ZN-8-517

Verlag: Convair, A Division of General Dynamics Corporation, San Diego, CA, 1959

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Approximately 2 inches thick. Marked CONFIDENTIAL--no longer classified based on subsequent Executive Orders and other national security guidance. Ink notation on front cover. First pages address the page/section changes made. Copy, perhaps mimeographed, one of multiple originals. The Table of Contents address: MA-1 and ASQ-25 Production Test Procedure, General Description; Pre-Installation Test Procedure (Part 2) Deleted; Pre-Installation Test Procedure (Part 1) Deleted; Post Installation Test and Harmonization Procedures; Pre-Flight Test Procedure; and Flight Test Procedures. No graphics observed. Convair, previously Consolidated Vultee, was an American aircraft-manufacturing company that later expanded into rockets and spacecraft. The company was formed in 1943 by the merger of Consolidated Aircraft and Vultee Aircraft. In 1953, it was purchased by General Dynamics, and operated as their Convair Division for most of its corporate history. Convair is best known for its military aircraft; it produced aircraft such as the Convair B-36 Peacemaker and Convair B-58 Hustler strategic bombers, and the Convair F-102 Delta Dagger and Convair F-106 Delta Dart interceptors. It also manufactured the first Atlas rockets. The company's subsequent Atlas-Centaur design continued this success and derivatives of the design remain in use as of 2023. In 1994, most of the company's divisions were sold by General Dynamics to McDonnell Douglas and Lockheed, with the remaining components deactivated in 1996. Heavy item that if sent outside of the U.S. requires additional shipping charges. The Convair F-106 Delta Dart was an all-weather interceptor aircraft designed and produced by the American aircraft manufacturer Convair. The F-106 was designed in response to the 1954 interceptor program. The F-106 was designed without a gun or provision for carrying bombs, instead carrying its AIM-4 Falcon air-to-air missiles within an internal weapons bay, its clean exterior was beneficial to supersonic flight. On 26 December 1956, the first prototype performed its maiden flight. After flight testing demonstrated lesser performance gains than anticipated, the USAF ultimately only ordered 350 of the planned 1,000 F-106s. Becoming operational in June 1959, the F-106 was the primary all-weather interceptor aircraft of the USAF through much of the Cold War era. During the 1960s, a competitive evaluation between the F-106 and the McDonnell Douglas F-4 Phantom II determined the latter to be marginally superior, yet the type continued to be operated for a further two decades due to extensive demand for the F-4 in other roles. In one high-profile incident over Montana on 2 February 1970, an unmanned F-106 recovered from a flat spin after its pilot had ejected, belly landing relatively intact in a snow-covered cornfield; it was recovered and continued to be flown for numerous years afterwards. The F-106 was gradually withdrawn from USAF service during the 1980s as the arrival of newer air superiority fighters, particularly the McDonnell Douglas F-15 Eagle, had made the role of dedicated interceptors obsolete. Numerous F-106s would be operated for a time by the Air National Guard. Many withdrawn aircraft were promptly converted into target drones and redesignated QF-106 under the Pacer Six program, which were used up in 1998. A handful of F-106s were operated by NASA for experimental purposes, such as the Eclipse Project, through to 1998. The F-106 used a Hughes MA-1 electronic guidance and fire control system. After takeoff, the MA-1 can be given control of the aircraft to fly it to the proper altitude and attack position. Then it can fire the Genie and Falcon missiles, break off the attack run and return the aircraft to the vicinity of its base. The pilot takes control again for the landing. ASQ-25 was an Airborne Weapon Control System manufactured by Hughes; used in F-101, F-102, F-106A/B. General Revision: Revised and Retyped complete Report; incorporated INTERIM CHA.…

Bestandsnummer des Verkäufers 88362

Bibliografische Details

Titel
Specification for F-106A/B Aircraft Weapon Control Systems; (Type MA-1 and ASQ-25) Production Alignment and Test Procedures Report ZN-8-517
Autor
Hollman, D. J. and Massie, L. E.
Verlag
Convair, A Division of General Dynamics Corporation, San Diego, CA
Erscheinungsjahr
1959
Zustand
Good
Einband
Three-hole punched binder

Ground Zero Books, Ltd.

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Verkäufer:in bei AbeBooks seit 14. August 1998

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