Remote Control Canard Missile with a Free-Rolling Tail Brake Torque System-Reference-Cited by-同舟云学术

Remote Control Canard Missile with a Free-Rolling Tail Brake Torque System

Published:1981-11 Issue:6 Volume:18 Page:550-555
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Blair A.B.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.57851

Reference6 articles.

1. 2Schult, E.D. "Free-Flight Measurements of the Rolling Effectiveness and Operating Characteristics of a Bellows-Actuated Split-Flap Aileron on a 60° Delta Wing at Mach Numbers Between 0.8 and 1.8,"NACARML54H17,Oct. 1954.

2. The Static and Magnus Aerodynamic Characteristics of the M823 Research Store Equipped with Fixed and Freely Spinning Stabilizers

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