Spinward Flow
SOC-14 5K
How is "spend extra fuel on reaction maneuvering" a contradiction of the powering down rule (under which you would presumably be performing minimal reactionless maneuvering anyway)?It directly contradicts the powering down rules
Changing the X axis parameter on the graph does not impact the Y axis parameter on that graph.
You might change the "area" described by a rectangle between (0,0) and the placement of (x,y) on the graph, altering a ship's overall fuel endurance profile when using fuel for reaction thrust to maneuver, but that doesn't "impact" the powering down rule at all or how the powering down rule functions (or when you would want to use it).
Note that under the modifications to the fuel rule proposed above, that would no longer be the case.E.g.: A 5000 Dt PP-1 LBB2 ship requires a 10 Dt fuel tank.
Your "5000 Dt PP-1 LBB2 ship" would require a 50 Dt fuel tank for 4 weeks of power plant operation plus reactionless maneuver capability within 1000 diameters of a gravity well. If you wanted to take that same ship beyond 1000 diameters and would therefore need to rely on HEPlaR reaction maneuvering capacity (as stipulated above) the ship would need to expend 2.5 Dt of fuel per day to maneuver beyond 1000 diameters. The HEPlaR reaction fuel could be drawn from the base 50 Dt allocation, reducing maximum endurance of power plant operation ... OR ... additional fuel tankage could be specified as part of the design and/or retrofitted after construction (demountable tanks, collapsible tanks, etc.) if needed to supply additional fuel reserves for use as reaction maneuver fuel beyond 1000 diameters for considerable durations.
Remember, MOST craft aren't going to spend a whole lot of their time in normal space beyond 1000 diameters of a gravity well. Some will ... such as Belters, Scouts, the occasional Lab Ship and the like either prospecting or conducting research of some kind, as well as some System Defense Boats on patrols ... but most craft will not be operated in such a way as to need extensive reaction mass for continuous acceleration beyond 1000 diameters of a gravity well.
In practical terms, most starships will not need more than about a 7-8 day HEPlaR reaction maneuvering fuel reserve under most circumstances simply because it would be faster to micro-jump (stay in same hex, but consume fuel as if performing a jump-1) a distance that would take 8 days to maneuver in normal space within a system.
Fully fueled starships with Jump-1 and 2 parsecs of range could thus micro-jump to the Oort Cloud (well beyond 1000 diameters of anything), operate on HEPlaR reaction maneuvering fuel reserve except when "close" to a rendezvous with an object for prospecting, research, surveying work and still have sufficient fuel remaining to micro-jump back into the closer orbits to refuel and resupply safely. Such starships would presumably want to have a larger fuel fraction available for extended HEPlaR reaction maneuvering under such mission profile conditions, altering their fuel demands relative to those of a "core system" design starship that spends almost all of its time within 1000 diameters of gravity wells operating on reactionless maneuver thrust electrically driven by fusion power plant EP output alone (no extra fuel required to maneuver).
Interplanetary Travel Distance by Time and Acceleration
There's a reason why I published this reference.
When the paradigm changes and you don't alter your assumptions to match the changes in the paradigm you are extremely susceptible to drawing the WRONG conclusions with extreme confidence.