Investigation of Drag-Modulated Supersonic Inflatable Aerodynamic Decelerators for Sounding Rocket Payloads

Author:

Miller Matthew J.1,Steinfeldt Bradley A.1,Braun Robert D.1

Affiliation:

1. Daniel Guggenheim School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Reference28 articles.

1. BloetscherF. “Aerodynamic Deployable Decelerator Performance Evaluation Program—Phase II,” Goodyear Aerospace Corp., U.S. Air Force Flight Dynamics Lab. TR-67-25, June 1967.

2. “PEPP Ballute Design and Development,” NASA CR-66585, Sept. 1967.

3. LevyL. L. “Use of Drag Modulation to Limit the Rate at Which Deceleration Increases During Nonlifting Entry,” Ames Research Center, NASA TN-D-319, Sept. 1961.

4. Explicit Guidance of Ballistic Entry Using Improved Matched Asymptotic Expansions

5. RoseP. H.HayesJ. E. “Drag Modulation and Celestial Mechanics,” Advances in the Astronautical Sciences, Vol. 8, Plenum Press, New York, 1963, pp. 178–187.ADASA90065-3438

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