Journal of Aeronautics & Aerospace Engineering
Open Access

Research at rocket-space complex and orbiter with liquid propellant engines on HPT

3^rd International Conference and Exhibition on Mechanical & Aerospace Engineering

October 05-07, 2015 San Francisco, USA

Pauk Oleg Leonidovich

Air-Space Agency ��?Magellan��?, Ukraine

Posters-Accepted Abstracts: J Aeronaut Aerospace Eng

Abstract :

It is a review of criteria for the establishment of active orbital spacecraft, taking into account the analysis of aspects of the application of the propulsion system running on hydrogen peroxide and the possibility of its return to the Earth surface. As a result of research, the concept of creating a modern type of spacecraft maneuvering in orbit, returning unmanned orbiter in the embodiment of the Satellite Remote Sensing (SRS) was proposed. In the report, the results of optimizing the design of the Launch Vehicle (LV) are reflected. This article examines the preceding schematic design elements of space rocket complex. In particular, the elements of LV, Orbiter, and their propulsion systems. Initial calculations of the aerodynamic parameters of Orbiter on the descent and maneuvering in low orbit were carried out. The report shows an embodiment of space rocket engine liquid propellant components that were selected.

Biography :

Email: alexander.levenko@gmail.com