FIELD: transport.
SUBSTANCE: in compliance with the proposed method, the rocket is arranged above the airframe and furnished with a wing-parachute. Separation and lifting the rocket off the aircraft result from combined action of the wing-parachute lift and forces of inertia created by effecting the steep climb maneuver whereat smaller area of the wing-parachute is required. The first stage mid-flight engine is started at a safe distance from the aircraft. At the instant of starting the engine, the wing-parachute is detached from the rocket, and the rocket is stabilised relative to its programmed trajectory. The proposed arrangement of the rocket of the aircraft allows using larger size and weight rockets to place payloads into orbit compared with arrangement of the payload in the aircraft freight compartment or below its airframe.
EFFECT: greater payload weight to be placed into orbit.
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR MISSILE TAKE-OFF FROM AIRCRAFT FOR ORBIT INJECTION OF PAYLOAD | 2004 |
|
RU2289084C2 |
METHOD OF LAUNCHING ROCKET FROM AIRCRAFT TO PLACE PAYLOAD INTO ORBIT | 2008 |
|
RU2394201C2 |
SPACE TRANSPORTATION SYSTEM ON THE BASIS OF THE LIGHT, MIDDLE AND HEAVY CLASSES ROCKETS FAMILY WITH THE SPACE ROCKETS AERIAL LAUNCH FROM THE SURFACE-EFFECT AIRBORNE SHIP BOARD AND ITS FUNCTIONING METHOD | 2014 |
|
RU2659609C2 |
AIR LAUNCHING COMPLEX | 2023 |
|
RU2827435C1 |
AIRCRAFT ROCKET LAUNCH SITE FORMED ON BASIS OF SPACE-MISSION VEHICLE ADAPTED FROM TOPOL-M ICBM AND CARRIER AIRCRAFT IL-76MF FOR INSERTION OF SMALL SPACECRAFTS INTO FINAL ORBITS BY INSERTING SMV FROM AIRCRAFT USING COMBINED TRANSPORT-LAUNCHING PLATFORM AND LIFTING-STABILIZING PARACHUTE | 2016 |
|
RU2636447C2 |
MULTI-MODE AIRCRAFT-BOOSTER FOR AVIATION ROCKET SPACE COMPLEX | 1999 |
|
RU2175934C2 |
REUSABLE FIRST STAGE OF THE LAUNCH VEHICLE | 2022 |
|
RU2790569C1 |
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 |
METHOD OF PAYLOAD ORBITAL INJECTION BY REUSABLE SPACE TRANSPORT VEHICLE (VERSIONS) | 2006 |
|
RU2331551C2 |
SYSTEM OF INJECTION OF PAYLOAD INTO LOW-ALTITUDE NEAR-EARTH ORBIT | 1997 |
|
RU2191145C2 |
Authors
Dates
2008-09-20—Published
2006-08-28—Filed