TY  - RPRT
TI  - Longitudinal Stability and Control Characteristics as Determined by the Rocket-model Technique for an Inline, Cruciform, Canard Missile Configuration with a Low-aspect-ratio Wing Having Trailing-edge Flap Controls for a Mach Number Range of 0.7 to 1.
AU  - Baber, Hal T , Jr
AU  - Moul, Martin T
PY  - 1955
UR  - https://ntrs.nasa.gov/citations/19930086337
ID  - 19930086337
ER  -