Launch vehicle with reconfigurable interstage propellant manifol

Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244172, B64G 100, B64G 140

Patent

active

051433281

ABSTRACT:
A launch vehicle having one or more high thrust solid propellant boosters and two or more liquid propellant stages all configured to burn in parallel and having an interstage propellant manifolding system between the parallel liquid burning stages. Preferably, existing U.S. launch vehicle stages may be employed as the parallel burning stages. An additional liquid stage burning in series with the lower stages may also be employed. The interstage propellant manifolding between the liquid burning stages allows the central vehicle core to be stabilized against high altitude wind loads and further provides increased performance to the launch vehicle. Additionally, the interstage propellant transfer manifold is equipped with a plurality of electromechanical valves to allow reconfiguration of the propellant flow in real time in the event of a stage failure, thereby providing significantly increased vehicle reliability.

REFERENCES:
patent: 2755046 (1956-07-01), Underwood, Jr.
patent: 3369771 (1968-02-01), Walley et al.
patent: 3782400 (1974-01-01), Hardison et al.
patent: 3934512 (1976-01-01), Adachi
patent: 3977633 (1976-08-01), Keigler et al.
patent: 4012012 (1977-03-01), Ligler
patent: 4104878 (1978-08-01), Chase
patent: 4451017 (1984-05-01), Marshall
patent: 4505124 (1985-03-01), Mayer
patent: 4591115 (1986-05-01), DeCarlo
patent: 4609169 (1986-09-01), Schweickert et al.
patent: 4723736 (1988-02-01), Rider
patent: 4796839 (1989-01-01), Davis
patent: 4807833 (1989-02-01), Pori
patent: 4834324 (1989-05-01), Criswell
Flight Performance Handbook for Powered flight Operations (Revised 1963) Ed. J. Frederick White, pp. 5-80 through 5-85.
"Predicting Launch Vehicle Failure" Aerospace America, Sep. 1989, pp. 36-46.
Titan Background Literature.
Delta Background Literature.
Atlas Background Literature.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Launch vehicle with reconfigurable interstage propellant manifol does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Launch vehicle with reconfigurable interstage propellant manifol, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Launch vehicle with reconfigurable interstage propellant manifol will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-763539

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.