Determine MUA distribution to maintain pressure in space

In summary, to determine the makeup air distribution and generate a pressurization map for three separate zones, you can use the Bernoulli's equation to calculate the pressure differences between the outside air supply and the required flow rates for each zone.
  • #1
Thao Hoang
1
0
hi,
i have a little side project that I'm currently stuck on.
there are three separate space/zone that is being supply by 10000 CFM of outside air. the min. requirement for each zone are: zone 1 need 2500 cfm, zone 2 need 1100 cfm, and zone 3 need 1300 cfm. A) determine the make up air distribution is needed to maintain pressure in each space. B) generate a pressurization map.
i know that i need to apply the bernoulli's to solve this problem but don't know where to start. any guidance is appreciated.
 
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  • #2
To solve this problem, you can start by using the Bernoulli's equation to calculate the pressure that is needed in each zone to ensure that the required CFM of outside air is supplied. For example, for Zone 1, you would need to calculate the pressure difference between the total outside air supply (10000 CFM) and the required flow rate of Zone 1 (2500 CFM). Once you have the pressure difference for each zone, you can then use this information to generate a pressurization map. This map should show how the pressure drops or increases as air moves from one zone to another.
 

FAQ: Determine MUA distribution to maintain pressure in space

1. What is MUA distribution and how does it affect pressure in space?

MUA distribution refers to the allocation of resources, specifically propellant, in a spacecraft to maintain a specific pressure in the cabin. It is important because pressure must be carefully regulated in space to ensure the safety and comfort of astronauts.

2. How do scientists determine the optimal MUA distribution for a spacecraft?

Determining the optimal MUA distribution involves complex calculations and simulations that take into account factors such as the size and weight of the spacecraft, the amount of propellant available, and the desired pressure in the cabin. It also requires careful consideration of potential variations and contingencies during the mission.

3. What are the potential consequences of an incorrect MUA distribution in a spacecraft?

An incorrect MUA distribution can have serious consequences for a spacecraft and its crew. If there is too much propellant allocated for maintaining pressure, the spacecraft may become too heavy and difficult to maneuver. On the other hand, if there is not enough propellant allocated, the pressure in the cabin may drop to unsafe levels, putting the crew at risk of decompression sickness.

4. How often is the MUA distribution adjusted during a space mission?

The MUA distribution is typically adjusted periodically throughout a space mission to account for changes in propellant levels and other factors. However, the frequency of adjustments may vary depending on the specific mission and spacecraft design.

5. Are there any alternative methods for maintaining pressure in space besides MUA distribution?

Yes, there are other methods for maintaining pressure in space, such as using mechanical systems or chemical reactions to generate oxygen. However, MUA distribution is often the most efficient and reliable method for regulating pressure in a spacecraft.

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