The LEO to GEO mission MDRE would have an Isp of about 1000 sec and carry a payload of more than 4000 tons, see APPENDICES A,E, and K. The asteroid retreival MDRE would bring back to high earth orbit Apollo- Amor or Earth Trojan (if discovered) asteroids weighing up to 10^6 to 10^7 tons for large scale space manufacturing efforts . Finally, the pulsed induction reaction engine could be used for the LEO to GEO transfer mission where a few tons of payload are involved, which are clearly too small for the classical MDRE.
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