Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5/

Main Author: Stone, Howard W.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration., Scientific and Technical Information Branch
Other Authors: Powell, Richard W.
Format: Book
Language:English
Published: Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984
Series:NASA technical paper 2283
Subjects:
ΒιβλιοθήκηΤαξιθετικός αριθμόςΑριθμός ΑντιτύπωνΠληροφορίεςΚατάσταση
Δημοκρίτειο Πανεπιστήμιο ΘράκηςTL 521 .31ΠροβολήOPAC