This chapter contains sections titled:
Conceptual Design of Winged Reusable Two‐Stage‐to‐Orbit Space Transport Systems
Background and Introduction
Concepts for Reusable Space Transports
Single‐Stage‐to‐Orbit SSTO
Two‐Stage‐to‐Orbit TSTO
Design Procedure
Design Tools and Methods
Baseline Concept
Boundary Conditions and Requirements
Variation of Mission and Staging Mach Number
Trade Studies
Evaluation and Comparison of the Concepts
Variation of Mission and Mach Numbers
Mission Comparison
Comparison of Mach Number Variation
Accelerator Vehicle Concepts
Trade Studies
Airbreathing Second Stage
LOX‐Collection
Comparison and Evaluation
Conclusion and Outlook
Evaluation and Multidisciplinary Optimization of Two‐Stage‐to‐Orbit Space Planes with Different Lower‐Stage Concepts
Introduction
Reference Configurations
Concept Design and Mission Requirements
Space Plane Configuration with Lifting Body Lower Stage
Space Plane Configuration with Waverider Lower Stage
Design and Optimization Parameters
Analysis Methods
Quality Criteria
Simulation and Optimization Software
Performance of Reference Space Planes
Mass Breakdown
Design Sensitivities
Optimization Results
Nominal Optimizations
Sensitivity‐Based Optimizations
Summary and Conclusions
Overall Design Aspects
09.05.2005
48 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Overall Architecture and Integration Aspects
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