Levenko Alexander Sergeyevich
Air-Space Agency, Magellan
Ukraine
Title: Research at rocket-space complex and orbiter with liquid propellant engines on HPT
Biography
Biography: Levenko Alexander Sergeyevich
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 his return to the Earth surface. As a result of research, was proposed the concept of creating a modern type of spacecraft - maneuvering in orbit returning unmanned orbiter in the embodiment of the satellite remote sensing (SRS). In a report reflects the results of optimizing the design of the Launch Vehicle (LV). Article examines the preceding schematic design elements of space rocket complex. In particular, the elements of LV, Orbiter, and their propulsion systems. Carried initial calculations aerodynamic parameters of Orbiter on the descent and maneuvering in low orbit. The report shows an embodiment of a space rocket engine liquid propellant components selected.