@misc{indiciaea39c6af8cc8d,
  title = {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.},
  author = {Baber, Hal T , Jr and Moul, Martin T},
  year = {1955},
  url = {https://ntrs.nasa.gov/citations/19930086337},
  note = {Source identifier: 19930086337}
}