FIELD: protection of spacecraft against anti-cosmic defense systems equipped with self-guidance means working in infra-red range; recoverable vehicles, hypersonic aircraft, missile nose cones, descent spacecraft.
SUBSTANCE: proposed method consists in forming protective screen around spacecraft which is cooled down to temperature of surrounding medium background. Used as protective screen is outer layer of spacecraft casing. Cooling the protective screen is effected by supplying the liquid nitrogen vapor at temperature of 77K into gap between envelope of fairing under which spacecraft is mounted on launch vehicle and outer layer of spacecraft casing.
EFFECT: extended field of application; enhanced efficiency of method.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR PROTECTION OF SPACE OBJECTS | 2008 |
|
RU2366594C1 |
| METHOD OF CAMOUFLAGING SPACE OBJECTS | 2008 |
|
RU2372578C1 |
| METHOD OF PROTECTION OF SPACECRAFT | 2005 |
|
RU2294866C1 |
| AMMUNITION FOR PASSIVE JAMMING COUNTERMEASURES FOR COMBINED HOMING HEADS OF "AIR-TO-AIR" AND "AIR-TO-GROUND" MISSILES | 2009 |
|
RU2412425C2 |
| AQUA AEROSPACE VEHICLE | 2012 |
|
RU2626418C2 |
| AEROSPACE AIRCRAFT | 2010 |
|
RU2436715C2 |
| PROTECTIVE MASKING SYSTEM | 1995 |
|
RU2075721C1 |
| METHOD AND SYSTEM FOR LONG-RANGE RADIO-ELECTRONIC RECONNAISSANCE BASED ON "TRACK IN ATMOSPHERE" "RADIO-INSIGHT" OBJECT FLYING IN STRATOSPHERE WITH HYPERSONIC SPEED | 2017 |
|
RU2689783C2 |
| INNER MULTILAYER HEAT INSULATION OF NOSE FAIRINGS | 2009 |
|
RU2410297C1 |
| SPACE-AIR DEFENSE COMPLEX | 2002 |
|
RU2227892C1 |
