NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Dynamic Tow Maneuver Orbital Launch TechniqueAn orbital launch system and its method of operation use a maneuver to improve the launch condition of a booster rocket and payload. A towed launch aircraft, to which the booster rocket is mounted, is towed to a predetermined elevation and airspeed. The towed launch aircraft begins the maneuver by increasing its lift, thereby increasing the flight path angle, which increases the tension on the towline connecting the towed launch aircraft to a towing aircraft. The increased tension accelerates the towed launch aircraft and booster rocket, while decreasing the speed (and thus the kinetic energy) of the towing aircraft, while increasing kinetic energy of the towed launch aircraft and booster rocket by transferring energy from the towing aircraft. The potential energy of the towed launch aircraft and booster rocket is also increased, due to the increased lift. The booster rocket is released and ignited, completing the launch.
Document ID
20150003296
Acquisition Source
Armstrong Flight Research Center
Document Type
Other - Patent
Authors
Rutan, Elbert L.
Date Acquired
March 19, 2015
Publication Date
May 20, 2014
Subject Category
Launch Vehicles And Launch Operations
Astrodynamics
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-13/914,744
Patent Number: US-Patent-8,727,264
Funding Number(s)
CONTRACT_GRANT: NND12AB91Z
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,727,264
Patent Application
US-Patent-Appl-SN-13/914,744
No Preview Available