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Mathematical Problems in Engineering
/
2016
/
Article
/
Tab 1
/
Research Article
The Multiobjective Trajectory Optimization for Hypersonic Glide Vehicle Based on Normal Boundary Intersection Method
Table 1
Important node in Pareto front of multiobjective optimization solution.
Pareto front
Minimum peak heat solution
Maximum terminal range solution
Range (km)
5597
6102
(W/cm
2
)
67.92
128.3