- #1
Dustin Maki
- 10
- 3
- TL;DR Summary
- If a spacecraft could keep station at the 2nd focus of Earth's orbit, what useful observations could be made?
If a hypothetical spacecraft could keep station at the 2nd focus of Earth's orbit, what useful observations could be made?
Each minute sees a new solar triangle Earth Sun Craft (ESC). Swept area remains constant, as should length SC, and length CE + ES.
With the Sun as our point source, and instrumentation at Earth and Craft we should be able to precisely measure angles between each of our objects.
Might the sum of those angles exceed 180degrees?
Presumably the craft could be repositioned at the 2nd focus of other solar orbits. Could there be a better vantage point to observe orbital mechanics?
If you had access to a craft with this capability, what would you want to do with it?
What physics and engineering challenges are the highest barriers to making such a craft real?
For example; assuming Raptor Vacuum engines are used for station keeping, approximately how many kilograms of methane and LOX would would be consumed for that purpose in 1 Earth year.
What is the expected hull temperature facing the Sun at that point in space?
Sorry for all the questions and no answers. They just occurred to me and I thought others might like to know the answers as well.
Each minute sees a new solar triangle Earth Sun Craft (ESC). Swept area remains constant, as should length SC, and length CE + ES.
With the Sun as our point source, and instrumentation at Earth and Craft we should be able to precisely measure angles between each of our objects.
Might the sum of those angles exceed 180degrees?
Presumably the craft could be repositioned at the 2nd focus of other solar orbits. Could there be a better vantage point to observe orbital mechanics?
If you had access to a craft with this capability, what would you want to do with it?
What physics and engineering challenges are the highest barriers to making such a craft real?
For example; assuming Raptor Vacuum engines are used for station keeping, approximately how many kilograms of methane and LOX would would be consumed for that purpose in 1 Earth year.
What is the expected hull temperature facing the Sun at that point in space?
Sorry for all the questions and no answers. They just occurred to me and I thought others might like to know the answers as well.