The fundamental flow mechanism is because of the pressure delta across the umbilical," Kshatriya said.
So, they don’t plan on using a pump, just thrust and inertia? I don’t get this at all? And won’t that leave a lot of the fuel in the tanker, especially on later launches?
And won’t that leave a lot of the fuel in the tanker, especially on later launches?
Not exactly sure what you mean here? Wouldn’t the amount of propellant left in the tanker depend mostly on the location of the “drain” between tanks? I’m also not clear why the problem would compound with multiple launches. Would you be able to clarify?
If a “natural” pressure differential is the only thing that’s transferring fuel, you can only ever average out the amount of fuel/pressure in both tanks. So if your craft is at 30%, and your tanker at 50%, a natural delta will result in both craft ending up with 40%.
I guess they want to settle the liquid fuel with ullage thrust, and then vent the gas in the craft, but not in the tanker, letting more flow into the craft? The article is very light on details.
Oh, yeah, I’m assuming they have to vent the ullage gas in the receiving tanker. Depending on the layout of the thrusters, they might even be able to utilize this gas to produce the some of the thrust during the propellant transfer.
So, they don’t plan on using a pump, just thrust and inertia? I don’t get this at all? And won’t that leave a lot of the fuel in the tanker, especially on later launches?
Not exactly sure what you mean here? Wouldn’t the amount of propellant left in the tanker depend mostly on the location of the “drain” between tanks? I’m also not clear why the problem would compound with multiple launches. Would you be able to clarify?
If a “natural” pressure differential is the only thing that’s transferring fuel, you can only ever average out the amount of fuel/pressure in both tanks. So if your craft is at 30%, and your tanker at 50%, a natural delta will result in both craft ending up with 40%.
I guess they want to settle the liquid fuel with ullage thrust, and then vent the gas in the craft, but not in the tanker, letting more flow into the craft? The article is very light on details.
Oh, yeah, I’m assuming they have to vent the ullage gas in the receiving tanker. Depending on the layout of the thrusters, they might even be able to utilize this gas to produce the some of the thrust during the propellant transfer.