Long, slender three-stage vehicle without fins throughout its length, the second stage of smaller diameter, joined to the first stage by a gradual truncated cone and ending with the third stage and payload on top. Nosecone with a sharp point. This construction was to afford the lowest airframe weight. First and second stage integral tanks are of aluminum w/riveted magnesium sheet skins. Second stage tanks are of stainless steel, aluminum frames and magnesium stringers and skin. Both first and second stages are of monocoque construction. Created by Smithsonian National Air and Space Museum Date Created 04/29/2022 Source Smithsonian National Air and Space Museum Keywords Cold War; Launch Vehicles; Rockets; Space Rights and Restrictions Not determined
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