Manned Spacecraft Design Principles
Auteur : Sforza Pasquale M.
Manned Spacecraft Design Principles presents readers with a brief, to-the-point primer that includes a detailed introduction to the information required at the preliminary design stage of a manned space transportation system.
In the process of developing the preliminary design, the book covers content not often discussed in a standard aerospace curriculum, including atmospheric entry dynamics, space launch dynamics, hypersonic flow fields, hypersonic heat transfer, and skin friction, along with the economic aspects of space flight.
Key concepts relating to human factors and crew support systems are also included, providing users with a comprehensive guide on how to make informed choices from an array of competing options. The text can be used in conjunction with Pasquale Sforza's, Commercial Aircraft Design Principles to form a complete course in Aircraft/Spacecraft Design.
PrefaceMission Specification1.Earth’s Atmosphere2.Hypersonic Missions in the Lower Atmosphere3.Atmospheric Entry Dynamics4.Space Launch Dynamics5.Hypersonic Flow Fields6.Hypersonic Heat Transfer and Skin Friction7.Spacecraft Configuration Design8.Safety, Reliability, and Risk Assessment9.Economic Aspects of Space Access
Appendices
System and subsystem engineers, spacecraft equipment designers, spacecraft operators, space scientists, students in aerospace engineering.
- Presents a brief, to-the-point primer that includes a detailed introduction to the information required at the preliminary design stage of a manned space transportation system
- Involves the reader in the preliminary design of a modern manned spacecraft and associated launch vehicle
- Includes key concepts relating to human factors and crew support systems
- Contains standard, empirical, and classical methods in support of the design process
- Culminates in the preparation of a professional quality design report
Date de parution : 11-2015
Ouvrage de 647 p.
19x23.3 cm
Thèmes de Manned Spacecraft Design Principles :
Mots-clés :
Ablation; Aerodynamic and reaction control systems; Air chemistry; Atmospheric entry; Atmospheric properties; Atmospheric tables; Ballistic coefficient; Boost trajectories; Catalytic wall; Cost estimating relationships; Crew flight safety; Earth orbits; Environmental control; Escape velocity; Failure rate models; Heat shield; Heat sink; Heat transfer; Hypersonic boundary layer and transition; Interplanetary trajectories; Launch abort systems; Launch systems; Life support systems; Lift-to-drag ra