FIELD: space-rocket engineering, applicable for destruction of natural and artificial space objects at high impact speeds. SUBSTANCE: the penetrating member is made of material with a porosity exceeding the porosity of material of the cylinder-shaped matrix with flat end faces by more than 1.5 times. EFFECT: enhanced cratering-crater depth and volume - at high speeds of impact as compared with monolithic strikers. 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COLLISION PROTECTING DEVICE | 2000 |
|
RU2260766C2 |
| DEVICE FOR WELL PERFORATION | 2001 |
|
RU2233969C2 |
| THERMOMECHANICAL CUTTING PROCESS | 2002 |
|
RU2266178C2 |
| EQUIPMENT FOR INVESTIGATING PLANE SHOCK WAVE PARAMETERS IN A POROUS MATERIAL | 0 |
|
SU586360A1 |
| DEVICE FOR DETERMINATION OF VISCOUS LIQUID FLOW VELOCITY PROFILE | 0 |
|
SU1140004A1 |
| TWO-STAGE LIGHT-GAS INSTALLATION | 2001 |
|
RU2251063C2 |
| METHOD OF ANALYSIS OF DISPERSED COMPOSITION OF POLYDISPERSED MATERIALS | 0 |
|
SU1536270A1 |
| METHOD OF MEASURING THIXOTROPY | 0 |
|
SU1179156A1 |
| METHOD FOR DETERMINING HEAT EXCHANGE COEFFICIENT OF SOLID BODIES | 1993 |
|
RU2046327C1 |
| ROTARY VISCOSIMETER | 0 |
|
SU1332193A1 |
