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Motion trajectories of the vehicle with mass injection pre-compressor cooling turbojet engines as the first stage of aircraft-space systems
- Authors: 1 11, 1 11
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 8, No 3-3 (2009): Special Issue
- Pages: 273-278
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/826
- DOI: https://doi.org/10.18287/2541-7533-2009-0-3-3(19)-273-278
- ID: 826
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Abstract
The motion of the vehicle with Mass Injection Pre-Compressor Cooling turbojet engines as the first stage of an aircraft-space system during the “steep – climb” maneuver is discussed. The aim of the maneuver is to climb at the preset inclination angle of the trajectory in order to launch a rocket with small payload into the low-earth orbit.
About the authors
1 1
Samara State Aerospace University
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
1 1
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
References
- Responsive Access Small Cargo Affordable Launch (RASCAL) Independent Performance Evaluation David Young AE8900 Special Project Report May 3, 2004 School of Aerospace Engineering Space System Design Laboratory Georgia Institute of Technology Atlanta, Georgia 30332-0150. http: // hdl. handle. net / 1853/8372.
- Балакин, В.Л. Траектории движения сверхзвукового самолёта как первой ступени авиационно-космической системы [Текст] / В.Л.Балакин, В.И.Потапов // Вестник Самарского государственного аэрокосмического университета. – 2009. – №1.
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