Fig. 1. Application of high energy pulsed solenoids with capacitor power
supply in a satellite swarm.

Conceptually it is considered that the problem has two components, the
foundational physics of multiple fields being wholly functional and the
physical components functioning in the proposed orbital environment.
Broad literature reviews have concluded that no singular aspect of
context or design prevents function so the proposed concept must be
viable by conclusion. The electromagnetic analysis of the proposed
interaction is the purpose of this paper, component technologies are
detailed before the design is assessed in relation to the problem.