System and method for improved air-launch of a launch vehicle from a towed aircraft
A launch system and method for orbital or suborbital air-launch of a payload involving releasably coupling a launch vehicle with a towed aircraft via an articulatable carriage to form an air-launch assembly, towing the air-launch assembly via a tow aircraft and interconnected tow cable to a first altitude, releasing the air-launch assembly from tow at or above the first altitude, activating the towed aircraft propulsion system and initiating a pull-up and climb maneuver of the towed aircraft to a second altitude, articulating the articulatable carriage to shift the air-launch assembly from a stowed position to a deployed position with the launch vehicle spaced from the towed aircraft, releasing the launch vehicle from the articulatable carriage and thus from the towed aircraft, and activating the launch vehicle propulsion system for further altitude gain or to meet specific mission requirements.
1 . A method of employing a launch system for orbital or suborbital air-launch of a payload, the method comprising the steps of:
releasably coupling a launch vehicle with a towed aircraft via an articulatable carriage to form an air-launch assembly, the articulatable carriage configured for selectively shifting the launch vehicle between a stowed position adjacent to the towed aircraft and a deployed position spaced from the towed aircraft, the launch vehicle having a launch vehicle central axis and the towed aircraft having a towed aircraft central axis;
configuring the air-launch assembly in the stowed position with the launch vehicle adjacent to the towed aircraft;
towing the air-launch assembly via a tow aircraft and interconnected tow cable to a first altitude;
releasing the air-launch assembly from tow at or above the first altitude;
activating a towed aircraft propulsion system and initiating a pull-up and climb maneuver of the towed aircraft to a second altitude;
after the steps of releasing the air-launch assembly from tow at or above the first altitude and activating the towed aircraft propulsion system and initiating the pull-up and climb maneuver of the towed aircraft to the second altitude, articulating the articulatable carriage to shift the air-launch assembly to the deployed position with the launch vehicle spaced from the towed aircraft and with the launch vehicle central axis at an inclined angle relative to the towed aircraft central axis in the range of one to ten degrees (1-10°);
releasing the launch vehicle from the articulatable carriage and thus from the towed aircraft; and
powering a launch vehicle propulsion system for further altitude gain or to meet specific mission requirements.
2 . The method of claim 1 comprising, prior to the step of towing the air-launch assembly, the further step of activating the towed aircraft propulsion system to provide take-off assist to the tow aircraft.
3 . The method of claim 1 comprising, prior to the step of releasing the air-launch assembly from tow at or above the first altitude, the further step of activating the towed aircraft propulsion system to allow for recovery of the air-launch assembly in the event of air-launch abortment.
4 . The method of claim 1 comprising, after the step of activating the towed aircraft propulsion system and prior to the step of articulating the articulatable carriage, the further step of turning off the towed aircraft propulsion system.
5 . The method of claim 4 wherein the step of turning off the towed aircraft propulsion system triggers the step of articulating the articulatable carriage.
6 . The method of claim 1 wherein the step of activating the towed aircraft propulsion system and initiating the pull-up and climb maneuver of the towed aircraft is such that the second altitude is more than 10,000 feet higher than the first altitude.
7 . The method of claim 1 wherein the articulatable carriage reaching the deployed position and the step of releasing the launch vehicle from the articulatable carriage occur substantially simultaneously.
8 . The method of claim 1 wherein the step of articulating the articulatable carriage comprises orienting the towed aircraft at a negative angle of attack relative to the launch vehicle.
9 . The method of claim 1 comprising, after the step of releasing the launch vehicle from the towed aircraft, the further step of executing an aerodynamic maneuver of the towed aircraft to further diverge the flight path of the towed aircraft from the flight path of the launch vehicle.
10 . The method of claim 1 wherein one or more of the steps are achieved via control system automation.
11 . The method of claim 1 comprising, prior to the step of releasably coupling the launch vehicle with the towed aircraft, the further step of assembling the launch vehicle on the articulatable carriage.