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High-Speed-Performance Analysis. Nominal and Optimal Boost Climb Performance Analysis

机译:高速性能分析。标称和最佳提升爬升性能分析

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Nominal and optimal boost climb trajectories were developed for an air-launched vehicle. The agreement between approximate nominal and exact numerical solutions was quite good. Three payoffs were addressed for the optimal trajectories; maximum speeds at burnout or apogee, minimum fuel to apogee, and minimum time to apogee. The last two are equivalent since the fuel-burning rate was constant. Thrust vectoring was considered for one problem, but the difference relative to zero thrust vectoring was negligible. The remaining problems only considered zero thrust vectoring. In general, the optimal angle-of-attack decreased with increasing time. The change was greater for the minimum time solution. For this case, a fast pitch-up occurred initially and then the angle-of-attack rapidly decreased to the angle-of-attack for -C sub LMAX. The gave the fastest pitch over to apogee. The minimum time solution may reach apogee before burn-out. This never occurs for the maximum speed case; the terminal condition is reached at or after burn-out. (Author)

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