Electromagnetic ground to orbit propulsion method and operating

Superconductor technology: apparatus – material – process – High temperature – per se – Having tc greater than or equal to 150 k

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

89 8, 124 3, 244 63, 335216, F41B 600

Patent

active

050933132

ABSTRACT:
A reusable and regenerative electromagnetic propulsion method and operating system is provided for propelling high mass payloads to orbital velocities which does not require a vacuum environment. The propulsion system comprises a self supporting superconducting dipole coil several kilometers in diamater that is accelerated by magnetic repulsive forces generated by a plurality of giant superconducting field coils mounted in the underground tunnels. The propulsion dipole is mounted inside a circular hypersonic wing-like structure equipped with movable aerodyanmic control surfaces for guidance. The propulsion system can accelerate a payload with any desired launch azimuth by accelerating along a line of magnetic induction generated by the field coils having the desired azimuth angle. The payload is attached to the propulsion system by a plurality of cables. After reaching orbital velocity, the payload is detached from the propulsion system and the propulsion system is decelerated back to the earth's surface by magnetic repulsive forces generated by the field coils. A large fraction of the orbital energy of the propulsion system is reconverted back into electrical energy by the inductive coupling between the magnetically decelerated propulsion coil and the field coils which is used to launch another payload.

REFERENCES:
patent: 4078747 (1978-03-01), Minovitch
patent: 4432333 (1984-02-01), Kurherr
patent: 4709883 (1987-12-01), Giuliani et al.
patent: 4939976 (1990-07-01), Minovitch
Bohn, E. V., Introduction to Electromagnetic Fields and Waves, 1968, pp. 213-220.
Kolm et al, "An Alternative Launching Medium", IEEE SPECTRUM, Apr. 1982, pp. 30-36.
Salkeld et al, "A Reusable Space Vehicle for Direct Descent from High Orbits", AIAA, Apr. 1981, pp. 46-47, 63.
Peaslee, Proceedings of the Impact Fusion Workshop, Jul. 10-12, 1979, Aug. 1979, pp. 213-217.
Hausmann et al, Physics, 1939, pp. 69.
Grob, Bernard, Basic Electronics, 1984, pp. 286-289.

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

Electromagnetic ground to orbit propulsion method and operating does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Electromagnetic ground to orbit propulsion method and operating , we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Electromagnetic ground to orbit propulsion method and operating will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-272214

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