@misc{indiciae2720281f8d0f,
  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 1.8},
  author = {Baber, H. T., Jr. and Moul, M. T.},
  year = {1955},
  url = {https://ntrs.nasa.gov/citations/19690067250},
  note = {Source identifier: 19690067250}
}