Abstract: | The purpose of this paper is, first, to review the over-all X-20A (Dyna-Soar) guidance requirements in terms of the present orbital program objectives and requirements; and second, to describe the functions of mechanization of the X-20A Primary Guidance Sybsystem is required to provide the following functions during X-20A ground launch missions (Fig. 1). |
Published in: | NAVIGATION: Journal of the Institute of Navigation, Volume 10, Number 3 |
Pages: | 247 - 265 |
Cite this article: | Scheidenheim, Ralph, "THE PRIMARY GUIDANCE SUBSYSTEM FOR THE X-20A (DYNA-SOAR) GLIDER", NAVIGATION: Journal of The Institute of Navigation, Vol. 10, No. 3, Fall 1963, pp. 247-265. |
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