The gravity well (the effects of gravity as a force eminating from the earth and the moon) as depicted (Earth, Moon and Sun) and hence the name of the site are so important that we set up a section devoted just to the physics of the well's impacts.
The tactics of space warfare in the extraterristal but near Moon space are also largely governed by the Well. The Gravity Well forces clear thinking about supply chains in Space.
Adding In Space Refueling (as in SpaceX's plans for its own purposes) makes the gravity well a force multiplier(many more craft of varying types for multiple missions simultaneously) by allowing for (a) stored fuel/refueling at the L-1 and L-2 points for the C&C Center as well as all the supporting offense and defense platforms, (2) in GEO/LEO points for the same, and (3) refueling all the various stations and weapon systems platforms on the Moon itself.
Hit the Down Arrow and See Gavity Well TACTICS DISCUSSION below
Check out the NOAA site (https://www.nesdis.noaa.gov/news/points-of-lagrange-satellite-million-miles-home) for the Lagrange Point (L-1, and L-2 thru 5) overview.
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1. One concept for military armament in the Gravity Well is for a constellation of Microsats.
a. One such configuration would be a Dual Satellite with a Payload Spacecraft and a Power Spacecraft joined by a metal carriage for launch and deployment.
Microsat and Carriage dimensions: 3 Feet high; 1 foot wide
b. Four Dual Satellites would be stacked on one side of a 12-foot central carriage for launch. The Launch Carriage would accommodate 16 satellites. A SpaceX Starship could launch two carriages thereby placing 32 Microsats in pre-positioned orbits within the Gravity Well. The Starship fairing and launch capacity is so large that another carriage and/or secondary payloads could be launched on the same ELV.
c. Payload satellites would include dual communications, printed circuit controller and power pack modules. Two miniature hydrazine propulsion tanks would allow both station-keeping and deployment to an enemy target satellite or capsule.
d. Power satellites would be attached to the Payload Satellite until a mission occurs. The Power Satellite would deploy twin 36-square-foot solar arrays capable of generating about 540 watts. A Sun finder sensor would continuously orient the Dual Satellites toward the Sun to ensure maximum power.
e. Payload satellites would accommodate a wide variety of payloads including, but not limited to the following: Communications packages, sensor suites, cameras, bombs/mines (eg: 3 Claymore mines on each satellite), obscurant propellant tanks and even dual “Locking Spears” with 12-foot cables to attach the Payload satellite to the enemy prior to weapon discharge.
f. Real-time video would be transmitted to either an orbiting or terrestrial command and control station on the Moon during the locking maneuvers and weapons discharge.
More than one Payload Satellite could attack an enemy target.
g. Enemy response would be difficult. The stealth Microsats are small enough to elude radars and would be camouflaged by the entire constellation. Enemy response would be very difficult, and any weapon discharge by an enemy would be a high-value projectile seeking a low-value American asset. The AI-smart constellation would sense an incoming projectile and disburse so the weapon would harmlessly pass through it.
2. Reconfigurable intelligent surfaces - A team of scientists from MPI-SP and RUB employed this technology to perform selective jamming. "You can think of the RIS device like a disco ball, which can reflect radio waves. The difference is that we can manipulate each mirror facet so that it directs the waves where we want them to," says Philipp Mackensen, lead author of this study. The team of researchers used the RIS system to successfully target just one of two devices, which were placed in very close proximity.