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Optimizing the propulsion of a hypersonic accelerator aircraft of a two-stage aerospace system
- Authors: Balakin V.L.1, Bebyakov A.A.1, Kotchyan A.G.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 7, No 1 (2008)
- Pages: 23-32
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/540
- DOI: https://doi.org/10.18287/2541-7533-2008-0-1(14)-23-32
- ID: 540
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Abstract
The paper deals with the propulsion of a hypersonic accelerator aircraft acting as the first stage of a two-stage aerospace system. Optimal and approximately optimal angle of attack programmes are defined on condition that fuel consumption is minimal. The impact of the trajectory inclination finite angle magnitude on the pattern of control programmes and mechanical trajectories is analysed.
About the authors
V. L. Balakin
Samara State Aerospace University
Author for correspondence.
Email: balakin@ssau.ru
Russian Federation
A. A. Bebyakov
Samara State Aerospace University
Email: balakin@ssau.ru
Russian Federation
A. G. Kotchyan
Samara State Aerospace University
Email: balakin@ssau.ru
Russian Federation
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