FIELD: transport facilities for recoverable vehicles.
SUBSTANCE: proposed system includes aero-space vehicle of aircraft configuration with ejector ramjet engines, recoverable spacecraft with rocket engine used as second stage and inter-orbital transport vehicle used as third stage. Provision may be also made for fourth stage for delivery of payload to geosynchronous orbit. Aero-space vehicle may be provided with auxiliary rocket boosters which is used in combination with re-entry and/or non-re-entry upper stages; it may be used for transportation of payload as hypersonic aircraft.
EFFECT: possibility of obtaining optimal flights from low to hypersonic speeds.
8 cl, 34 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SYSTEM OF INJECTION OF PAYLOAD INTO LOW-ALTITUDE NEAR-EARTH ORBIT | 1997 |
|
RU2191145C2 |
| AEROSPACE CRAFT WITH NUCLEAR PROPULSOR AND AEROSPACE FLIGHTS PERFORMED THEREBY | 2013 |
|
RU2574295C2 |
| SIMPLIFIED SHUTTLE MODULE FOR CARRIER ROCKET | 2011 |
|
RU2566597C2 |
| RECOVERABLE BOOSTER OF FIRST STAGE OF LAUNCH VEHICLE | 1999 |
|
RU2148536C1 |
| STAROVEROV'S SPACECRAFT (VERSIONS) AND/OR ALGORITHMS OF ITS OPERATION | 2012 |
|
RU2503592C1 |
| METHOD OF SERVICING COSMIC ARTICLES AND SHUTTLE AEROSPACE SYSTEM FOR ITS IMPLEMENTATION | 2007 |
|
RU2342288C1 |
| AIRCRAFT FOR INTERCONTINENTAL FLIGHTS IN THE STRATOSPHERE | 2021 |
|
RU2758725C1 |
| MEANS METHOD AND SYSTEM FOR LAUNCHING SPACECRAFT ON BASIS OF TOWED GLIDER | 1995 |
|
RU2175933C2 |
| AIRCRAFT MISSILE COMPLEX | 2005 |
|
RU2317923C2 |
| METHOD OF INJECTION OF OBJECTS INTO NEAR-EARTH ORBIT AND RECOVERABLE AERO-SPACE ROCKET AIRCRAFT-CARRIER FOR REALIZATION OF THIS METHOD (AERO-SPACE SYSTEM NUR-SAID SYSTEM) | 2001 |
|
RU2232700C2 |
