Large heat load are encountered in hypersonic flight applications due to the high vehicle
speed (over Mach 5, ie 5000kmh− 1) and to the combustion heat release. If passive and …

'Estr total energy stored in the control volume, W 'Ew, corr correct heat § ux on the chamber
wall, W/m2 h external combustion chamber height, m J momentum § ux ratio m mass, kg OF …

The development of hypersonic vehicles (up to Mach 10) leads to an important heating of
the whole structure. The fuel is thus used as a coolant. It presents an endothermic …

Large heat load are encountered in hypersonic and space flight applications due to the high
vehicle speed (over Mach 5, ie 5000kmh− 1) and to the combustion heat release. If passive …

TO ENSURE the thermal resistance of hypersonic structures, active cooling techniques are
of interest, notably in the case of regenerative methods to be applied on the scramjet engine …

With the demand of faster transport in aviation industry and more cost-efficient operation of
space flights the interest in propulsion for supersonic and hypersonic flight steadily grew …

I. Introduction or high-speed aircraft, material and cooling issues for both airframe and
engine are one of the key elements which force the designer to limit the flight Mach number …

With the demand of faster transport in aviation industry and more cost-efficient flight
operation, the interest in propulsion for supersonic and hypersonic flight steadily grew in the …

Todays' high performance liquid propellant rocket engines are mainly operated with the
cryogenic propellant combination LOX/LH2, due to the high specific impulse. The …

Alongside with the demand of faster transport in aviation industry and more cost-efficient
operation of space flights the interest in propulsion for supersonic and hypersonic flight grew …