Since Heiwa is refusing to show us the message he sent to NASA (or just can't understand what is being asked of him), I wonder if we can file a freedom of information request to see what he said.
Assuming he's not just making it all up.
No, I am hard at work to update my web page about it.
Lagrange points are positions in space where the gravitational forces of a two-body system like the Sun and Earth produce enhanced regions of attraction and repulsion.
These can be used by spacecraft as "parking spots" in space to remain in a fixed position with minimal fuel consumption, if you can find them, I am told.
The ESA/NASA clowns suggest that the JWST can orbit (!!) around Lagrange Point L2.
It is called a halo orbit, a periodic, three-dimensional orbit near one of the L1, L2 or L3 Lagrange points in the three-body problem of orbital mechanics.
Although a Lagrange point is just a point in empty space, its peculiar characteristic is that it can be orbited by a Lissajous orbit or a halo orbit, I am told.
In orbital mechanics, a Lissajous orbit is a quasi-periodic (?) orbital trajectory that an object like the JWST can follow around a Lagrangian point of no mass in a three-body system without requiring any propulsion.
So Lagrangian points exist in a two-body system. When you enter a third body, like the JWST, into this system it becomes a three-body dynamic system and the third body can Lissajous orbit around the Lagrangian point requiring no propulsion, of course, I am told.
Questions remain how to enter the JWST in a Lissajous orbit around Lagrange point L2 and what the orbit sped and radius are.
It seems the JWST will change direction all the time around L2, so if you shall observe the end of the Universe from L2 you have to change your aim all the time. How to do it?
I have asked ESA/NASA about it and await a reply.