Physical frameworks of safe vehicles for space tourism

The attention to specific problems of guarantee of sub-orbital flight safety is accented. It is displayed, that physical limitations on ascent and reentry segments form conflict requirements to configurations of the launcher and reentry vehicle. The algorithm of construction of permissible parameter ranges determining a shape of such vehicles and their critical flight regimes is offered. The developed technique is demonstrated as an application to analyze a possibility to use the launcher Angara-1 for space tourism purposes.