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Development of the German A-4 guidance and control system, 1939 - 1945: A memoirThe development by 1943 of a fully inertial navigational system for the German A-4 (V-2) missile is detailed. This flight control system used a triple-axis stabilized platform with two longitudinal accelerometers and one lateral accelerometer.
Document ID
19770026117
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Steinhoff, E. A. (New Mexico Research Inst., Inc. Alamogordo, NM, United States)
Date Acquired
August 8, 2013
Publication Date
September 1, 1977
Publication Information
Publication: NASA, Washington Essays on the History of Rocketry and Astronautics, Vol. 2
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
77N33061
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19770026104Collected WorksEssays on the History of Rocketry and Astronautics: Proceedings of the Third Through the Sixth History Symposia of the International Academy of Astronautics, Volume 219770026104Collected WorksEssays on the History of Rocketry and Astronautics: Proceedings of the Third Through the Sixth History Symposia of the International Academy of Astronautics, Volume 2
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