Abstract
As described in the previous chapter, Japan’s quest for the development of an indigenous launch capability began with the pioneering efforts of Itokawa and his team at IIS in the 1950s and at ISAS in the 1960s. Their program to develop solid propellant vehicles (Kappa, Lambda, Mu) for launching mini satellites to low earth orbit was thwarted in the late 1960s by three consecutive technological failures along with ongoing internal problems. These setbacks left the field open for the rival solid- and liquid-fuel program being undertaken by the NSDC, which progressed from developing a three-stage Q rocket in the 1960s to an N series constructed with American help in the 1970s. This was established with an intergovernmental agreement in which Washington undertook “to provide to the Japanese Government or to Japanese industry under contract with the Japanese Government, unclassified technology and equipment […] for the development of Japanese Q and N launch vehicles and communications and other satellites for peaceful purposes.”1 This chapter focuses on the circumstances leading up to this arrangement, which was strongly promoted by the State Department, and the difficulties that NASA faced in interpreting its scope, and in cooperating with its implementation. That experience, in turn, enabled Japan to develop a “homegrown” H series of rockets in the 1980s, the latest being H-IIA capable of placing application satellites weighing more than two tons in geosynchronous orbit.2
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Notes
For a nuts and bolts history of the development of Japanese H series rocket, see T. Godai, “H-II: A New Launch Vehicle in the 1990’s,” Acta Astronautica 14 (1986), 143–157;
I. Hiraki and Y. Takenaka, “Development of Launch Vehicles for Application Purposes,” Acta Astronautica 7:8–9, 967–977;
A. Konno, M. Endo, Y. Koyari, and Y. Yamada, “Development Status of H-II Rocket Cryogenic Propulsion Systems,” Acta Astronautica 28 (1992), 127–134;
K. Noda and M. Endo, “H-IIA rocket program,” Acta Astronautica 45:10 (1999), 639–645;
R. Sekita, A. Watanabe, K. Hirata, and T. Imoto, “Lessons Learned from H-2 Failure and Enhancement of H-2A Project,” Acta Astronautica 48:5–12, 431–438;
K. Tomioka and Y. Kohsetsu, “H-II Launch Vehicle Development Status in Terms of Vibration, Shock and Acoustic,” Acta Astronautica 22 (1990), 43–48.
Arms Control and Disarmament Agency, “Space Cooperation with Japan: Arms Control Considerations,” September 6, 1966, in John M. Logsdon, Learning from the Leader: The Early Years of U.S. Japanese Cooperation in Space (undated, unpublished paper), Space Policy Institute, George Washington University, Washington, DC, 7.
John M. Logsdon, ed., Exploring the Unknown: Selected Documents in the His tory of the U.S. Civil Space Program, Vol. 2, External Relationships (Washington, DC: NASA SP-4407, 1996), 46.
Yasushi Sato, “Local Engineering in the Early American and Japanese Space Programs: Human Qualities in Grand System Building,” PhD dissertation, University of Pennsylvania, 2005, 334.
Steven J. Isakowitz, et al., International Reference Guide to Space Launch Systems (Reston, VA: American Institute of Aeronautics and Astronautics), 2004, 185.
Ka Zeng, Trade Threats, Trade Wars. Bargaining, Retaliation, and American Coercive Diplomacy (Ann Arbor: University of Michigan Press, 2004), 152.
Ronald A. Cass, “Velvet Fist in an Iron Glove. The Omnibus Trade and Competitiveness Act of 1988,” Regulation (Winter 1991), 50–56, at 52.
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© 2013 John Krige, Angelina Long Callahan, and Ashok Maharaj
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Krige, J., Callahan, A.L., Maharaj, A. (2013). NASA and the Politics of Delta Launch Vehicle Technology Transfer to Japan. In: NASA in the World. Palgrave Studies in the History of Science and Technology. Palgrave Macmillan, New York. https://doi.org/10.1057/9781137340931_10
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DOI: https://doi.org/10.1057/9781137340931_10
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