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Fundamentals of Decompression ENAE 697 - Space Human Factors and Life Support U N I V E R S I T Y O F MARYLAND Fundamentals of Decompression • History Tissue models – Haldane – Workman – Bühlmann Physics of bubbles Spacecraft cabin atmospheres 1 © 2011 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu

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Page 1: Fundamentals of Decompressionspacecraft.ssl.umd.edu/academics/697S11/697S11L07... · Fundamentals of Decompression ENAE 697 - Space Human Factors and Life Support U N I V E R S I

Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Fundamentals of Decompression• History• Tissue models

– Haldane– Workman– Bühlmann

• Physics of bubbles• Spacecraft cabin atmospheres

1

© 2011 David L. Akin - All rights reservedhttp://spacecraft.ssl.umd.edu

Page 2: Fundamentals of Decompressionspacecraft.ssl.umd.edu/academics/697S11/697S11L07... · Fundamentals of Decompression ENAE 697 - Space Human Factors and Life Support U N I V E R S I

Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

First Class Assignment• Four topics in the first section of the course

– Space Habitability– Human Factors – Anthropometrics– Psychosocial Aspects

• Find a technical paper in two of the topic areas• Post the paper (in PDF) and a summary (~0.5-1

page) to discussion board on Blackboard• No duplication! There’s an advantage in being first• Due Thursday March 3rd

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Discussion of Term Project• Please go to Blackboard site and list team members

(and innovative team names) for all teams• First phase: design interior layout of X-Hab in

configuration for 2011 test series– Accommodations for four crew– Diagrams coming for outer envelope

• Submit as slide package (no presentation) by March 18 (i.e., before Spring break)

• Second phase: full interior layout of two layers with life support and habitat elements

3

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Caissons• Pressurized chambers

for digging tunnels and bridge foundations

• Late 1800’s - caisson workers exhibited severe symptoms– joint pain– arched back– blindness– death

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Brooklyn Bridge• Designed by John Roebling, who

died from tetanus contracted while surveying it

• Continued by son Washington Roebling, who came down with Caisson Disease in 1872

• Competed by wife Emily Warren Roebling

• 110 instances of caisson disease from 600 workers

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Decompression Sickness (DCS)• 1872 - Dr. Alphonse Jaminet noted similarity

between caisson disease and air embolisms• Suggested procedural modifications

– Slow compression and decompression– Limiting work to 4 hours, no more than 4 atm– Restricting to young, healthy workers

• 1908 - J.B.S. Haldane linked to dissolved gases in blood and published first decompression tables

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Supersaturation of Blood Gases• Early observation that “factor of two” (50% drop in

pressure) tended to be safe• Definition of tissue ratio R as ratio between

saturated pressure of gas compared to ambient pressure

• 50% drop in pressure corresponds to R=1.58(R values of ~1.6 considered to be “safe”)

7

R =PN2

Pambient= 0.79 (nominal Earth value)

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Tissue Models of Dissolved Gases• Issue is dissolved inert gases (not involved in

metabolic processes, like N2 or He)• Diffusion rate is driven by the gradient of the

partial pressure for the dissolved gas

where k=time constant for specific tissue (min-1)P refers to partial pressure of dissolved gas

8

dPtissue(t)dt

= k [Palveoli(t)− Ptissue(t)]

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Solution of Dissolved Gas Diff. Eq.• Assume ambient pressure is piecewise constant

(response to step input of ambient pressure)• Result is the Haldane equation:

• Need to consider value of Palveoli

where Q=fraction of dissolved gas in atmosphere ΔPO2=change in ppO2 due to metabolism

9

Ptissue(t) = Ptissue(0) + [Palveoli(0)− Ptissue(0)]�1− e−kt

Palveoli =�

Pambient − PH2O +1−RQ

RQPCO2

�Q

Palveoli = (Pambient − PH2O − PCO2 + ∆PO2)Q

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Linearly Varying Pressure Solution• Assume R is the (constant) rate of change of

pressure - solution of dissolved gases PDE is

• This is known as the Schreiner equation • For R=0 this simplifies to Haldane equation• Produces better time-varying solutions than

Haldane equation• Easily implements in computer models

10

Pt(t) = Palv0 + R

�t− 1

k

�−

�Palv0 − Pt0 −

R

k

�e−kt

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Tissue Saturation following Descent

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Tissue Saturation after Ascent

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Effect of Multiple Tissue Times

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Haldane Tissue Models• Rate coefficient frequently given as time to evolve

half of dissolved gases:

• Example: for 5-min tissue, k=0.1386 min-1• Haldane suggested five tissue “compartments”: 5,

10, 20, 40, and 75 minutes• Basis of U. S. Navy tables used through 1960’s• Three tissue model (5 and 10 min dropped) • 1950’s: Six tissue model (5, 10, 20, 40, 75, 120)

14

T1/2 =ln (2)

kk =

ln (2)T1/2

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Workman Tissue Models• Dr./Capt. Robert D. Workman of Navy

Experimental Diving Unit in 1960’s• Added 160, 200, 240 min tissue groups• Recognized that each type of tissue has a differing

amount of overpressure it can tolerate, and this changes with depth

• Defined the overpressure limits as “M values”

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Workman M Values• Discovered linear relationship between partial

pressure where DCS occurs and depth

M=partial pressure limit (for each tissue compartment)M0=tissue limit at sea level (zero depth)ΔM=change of limit with depth (constant)d=depth of dive

• Can use to calculate decompression stop depth

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M = M0 + ∆Md

dmin =Pt −M0

∆M

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

PADUA (Univ of Penn.) Tissue ModelTissue T1/2 (minutes) M0 (bar)

1 5 3.0402 10 2.5543 20 2.0674 40 1.6115 80 1.5816 120 1.5507 160 1.5208 240 1.4909 320 1.490

10 480 1.459

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Bühlmann Tissue Models• Laboratory of Hyperbaric Physiology at University

Hospital, Zurich, Switzerland• Developed techniques for mixed-gas diving,

including switching gas mixtures during decompression

• Showed role of ambient pressure on decompression (diving at altitude)

• Independently developed M-values, based on absolute pressure rather than SL depth

• “Zurich” 12 and 16-tissue models widely used

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Bühlmann M-Value Models• Modifies Workman model by not assuming sea

level pressure at water’s surface

Pamb=pressure of breathing gasb=ratio of change in ambient pressure to change in tissue pressure limit (dimensionless)a=limiting tissue limit at zero absolute pressure

• ZH-L16 model values for a and b

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M =Pamb

b+ a

a = 2 T− 1

31/2 < bar > b = 1.005− T

− 12

1/2

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Physics of Bubbles• Pressure inside a bubble is balanced by exterior

pressure and surface tension

where γ=surface tension in J/m2 or N/m (=0.073 for water at 273°K)

• Dissolve gas partial pressure Pg=Pamb in equilibrium

• Gas pressure in bubble Pint>Pamb due to γ• All bubbles will eventually diffuse and collapse

20

Pinternal = Pambient + Psurface = Pambient +2γ

r

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Critical Bubble Size• Minimum bubble size is defined by point at which

interior pressure Pint = gas pressure Pg

• r<rmin - interior gas diffuses into solution and bubble collapses

• r>rmin - bubble will grow • r=rmin - unstable equilibrium

21

rmin =2γ

Pg − pambient

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Bubble Formation and Growth• In equilibrium, external pressure balanced by internal

gas pressure and surface tension• Surface tension forces inversely proportional to radius

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

“Clinical” Discussion of DCS• Tissue models are predictive, not definitive• Every individual is different

– Overweight people more susceptible to DCS– Tables and models are predictive limits - there will be

“outliers” who develop DCS while adhering to tables

• Doppler velocimetry reveals prevalence of bubbles in bloodstream without presence of DCS symptoms - “asymptomatic DCS”

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Implications of DCS in Space Flight• Drop from sea level pressure to ~4 psi, 100% O2

pressure– Equivalent to ascent from fully saturated 120 ft dive – Launch in early space flight– Extravehicular activity from shuttle or ISS

• To have “safe” (R=1.4) EVA from shuttle requires suit pressure of 8.2 psi

24

R =PN2

Pamb=

14.7(0.78)4

= 2.87

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Current Denitrogenation Approaches• Depress to 10.2 psi for 12-24 hours prior to EVA

– Full cabin depress in shuttle– “Campout” in air lock module of ISS

• Exercise while breathing 100% O2• In-suit decompression on 100% O2 (3.5-4 hours)

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Historical Data on Cabin Atmospheres

26

from Scheuring et. al., “Risk Assessment of Physiological Effects of Atmospheric Composition and Pressure in Constellation Vehicles” 1 6th Annual Humans in Space, Beijing, China, May 2007

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Spacecraft Atmosphere Design Space

27

from Scheuring et. al., “Risk Assessment of Physiological Effects of Atmospheric Composition and Pressure in Constellation Vehicles” 1 6th Annual Humans in Space, Beijing, China, May 2007

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Effect of Pressure and %O2 on Flammability

28

from Hirsch, Williams, and Beeson, “Pressure Effects on Oxygen Concentration Flammability Thresholds of Materials for Aerospace Applications” J. Testing and Evaluation, Oct. 2006

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Atmosphere Design Space with Constraints

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from Scheuring et. al., “Risk Assessment of Physiological Effects of Atmospheric Composition and Pressure in Constellation Vehicles” 1 6th Annual Humans in Space, Beijing, China, May 2007

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Fundamentals of DecompressionENAE 697 - Space Human Factors and Life Support

U N I V E R S I T Y O FMARYLAND

Constellation Spacecraft Atmospheres

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from Scheuring et. al., “Risk Assessment of Physiological Effects of Atmospheric Composition and Pressure in Constellation Vehicles” 1 6th Annual Humans in Space, Beijing, China, May 2007