FIELD: transport.
SUBSTANCE: invention relates to cosmonautics and can be used for safeguarding Earth against collision with dangerous cosmic body. Moon launch missile system comprises launching table located directly on the Moon surface, thermal casing placed on launching table and having opening cover at the top, mirrored outer surface and inner surface covered with heat insulating material (teflon, polytetrafluoroethylene, polychlorotrifluoroethylene, crystalline copolymer of ethane with tetrafluoroethylene), temperature-control system with heat accumulators and heater, power source, jet-propulsion solid-fuel missile with payload of 5-9 tons and takeoff mass of 20-30 tons. The launching table in the central part has translating cover to exhaust gases during missile takeoff.
EFFECT: invention permits to improve the Earth safety against collision with dangerous cosmic body.
6 cl
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF HEATING OF LUNAR ROCKET LAUNCHER COMPLEX | 2012 |
|
RU2539675C2 |
| METHOD OF HEATING THE LUNAR ROCKET LAUNCHER COMPLEX | 2012 |
|
RU2511746C2 |
| CONTROL SUPPORT CENTRE FOR ASTEROIDAL SAFETY SYSTEM | 2012 |
|
RU2518504C2 |
| METHOD FOR TRANSFER OF WORKING FLUID FOR ENGINES OF SPACECRAFTS AND SYSTEM OF ITS IMPLEMENTATION | 2009 |
|
RU2385275C1 |
| INSTALLATION TO LAUNCH ROCKETS FROM MOON AND METHOD OF PREPARING ROCKET FOR LAUNCHING | 2007 |
|
RU2354593C1 |
| ROCKET-SPACE SYSTEM | 1993 |
|
RU2087389C1 |
| ROCKET LAUNCH COMPLEX WITH A ROCKET-CATAPULT VEHICLE FOR FLIGHTS TO THE MOON AND BACK | 2020 |
|
RU2743061C1 |
| METHOD OF CONTROL OF SPACE ROCKET COMPLEX | 1996 |
|
RU2108540C1 |
| METHOD OF ACCUMULATING SPACESHIP POWER SUPPLY | 2010 |
|
RU2451631C1 |
| METHOD OF DESTRUCTION OF OBJECTS CONTAINING NUCLEAR SUBSTANCES | 1990 |
|
RU2041140C1 |
