Longitudinal Characteristics at Transonic and Supersonic Speeds of a Rocket-propelled Airplane Model Having a 60 Degree Delta Wing and Low Swept Horizontal Tail (1955)
NASA Technical Reports Server (NTRS) · leaf 21
NACA RM L55F27 20 … L-83125 Figure 2.- Model and booster on launcher.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
