Opening book details…
About this nonfiction
Effects of relaxed static longitudinal stability on a single-stage-to-orbit vehicle design by Freeman, Delma C. is a nonfiction available to read on EtoBox.
It is typically read by self-directed learners exploring a subject in depth.
Common subject areas: history, science, philosophy, social sciences.
- Author
- Freeman, Delma C.
- Publisher
- National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1979.
- Published
- 1979
- Language
- EN
- Category
- nonfiction
More by Freeman, Delma C.
Browse all works by Freeman, Delma C.
Similar books
- Static aerodynamic characeristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63 / Delma C. Freeman, Jr. and Roger H. Fournier, Langley Research Center. — Delma C. Freeman (1978)
- Dynamic Stability Characteristics of the Combination Space Shuttle Orbiter and Ferry Vehicle / Delma C. Freeman, Jr. and Richmond P. Boyden. — Delma C. Freeman (1977)
- Notes on the Static Longitudinal Stability and Control of Aircraft. — Brehaus, Waldemar Otto, 1918- (1953)
- Abort Performance for a Winged-body Single-stage to Orbit Vehicle — Jeffrey A. Lyon (1995)
- Comparison of Space Shuttle Orbiter Low-speed Static Stability and Control Derivatives Obtained from Wind-tunnel and Approach and Landing Flight Tests / Delma C. Freeman, Jr., and Barnard Spencer, Jr. — Delma C. Freeman (1980)
- Thermal Effects on Static Aeroelastic Stability and Control. — Bell Aircraft Corporation (1959)