aerospace physiology
TRANSCRIPT
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Aerospace Physiology• Lecture #14 – October 14, 2021 • Cardiopulmonary physiology
– Respiratory – Cardiovascular
• Musculoskeletal • Vestibular • Neurological • Environmental Effects
1
© 2021 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
The Human Respiratory System
2
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Lung Measurements
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1985
3
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Metabolic Processes• Respiratory Quotient (“RQ”)
• Function of activity and dietary balance – Sugar: – Protein: – Fat:
• For well-balanced diet, RQ~0.85
4
RQ = Exhaled volume of CO2Inhaled volume of O2
C6H12O6 + 6O2 → 6CO2 + 6H2O (RQ = 1.0)2C3H7O2N + 6O2 → 5CO2 + 5H2O (RQ = 0.83)C57H104O6 + 80O2 → 57CO2 + 52H2O(RQ = 0.71)
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
VO2 Metabolic Workload Measurement
5
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
VO2 Measurement in (Simulated) Suit
6
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
The Human Circulatory System
7
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Blood Pressure in Circulatory System
8
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Gas Exchange in the Lungs
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1985
9
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Gas Exchange in the Tissues
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1985
10
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Respiratory Problems• Hypoxia
– Hypoxic – Hypemic – Stagnant – Histotoxic
• Hyperoxia • Hypocapnia • Hypercapnia
11
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Types of Hypoxia• Hypoxic (insufficient O2 present)
– Decompression – Pneumonia
• Hypemic (insufficient blood capacity) – Hemorrhage – Anemia
• Stagnant (insufficient blood transport) – Excessive acceleration – Heart failure
• Histotoxic (insufficient tissue absorption) – Poisoning
12
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Pressure Effects on Blood Oxygenation
13
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1996
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Pressure Effects on Blood Oxygenation
14
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1996
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Effects of Supplemental Oxygen
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1985
15
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Hypoxia Effective Performance Time
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1985
16
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Lung Overpressure Following Decompression
17
From Nicogossian and Gazenko, Space Biology and Medicine - Volume II: Life Support and Habitability, AIAA 1994
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Oxygen Toxicity
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1985
18
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Effects of ppCO2
19
From James T. Joiner, NOAA Diving Manual, Fourth Edition, 2001
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Acute Effects of Hyperventilation
20
From James T. Joiner, NOAA Diving Manual, Fourth Edition, 2001
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Gravity Effects on Arterial Pressure
120/80 mmHg
95/55 mmHg
210/170 mmHg
320 mm
1200 mm
1000 mmH2O = 74.1 mmHg
21
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Acceleration Effects on Arterial Pressure
120/80 mmHg
25/–– mmHg
475/435 mmHg
320 mm
1200 mmAt 4 g’s longitudinal: 1000 mmH2O = 296 mmHg
22
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Cardiovascular Effects of Microgravity• Cardiovascular deconditioning • Upper body blood pooling • Changes in blood volume • Increased calcium content
23
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
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”)
24
R =PN2
Pambient= 0.79 (nominal Earth value)
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
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
25
dPtissue(t)dt
= k [Palveoli(t)� Ptissue(t)]
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Solution of Dissolved Gas Differential Eqn.
• 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
26
Ptissue(t) = Ptissue(0) + [Palveoli(0)� Ptissue(0)]�1� e�kt
⇥
Palveoli =�
Pambient � PH2O +1�RQ
RQPCO2
⇥Q
Palveoli = (Pambient � PH2O � PCO2 + �PO2)Q
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Alveolar Pressure Corrections• At body temperature (37°C=98.6°F), 100%
humidified air has a partial pressure of 47 mmHg=6.3 kPa=0.91 psi – this is independent of total pressure or atmospheric composition
• Earth atmosphere=78% N2=Q, 0.04% CO2 (ISS limit ≤0.5% (negligible for these calculations)
•
•
PN2,alveoli(sea level) = (14.7 − 0.97) 0.78 = 10.7 psiPN2,alveoli(8.2 psi/32 % O2) = (8.2 − 0.97) 0.68 = 4.9 psi
27
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Scuba Diving Decompression
28
05
101520253035404550
0 20 40 60 80 100 120 140 160
Tiss
ue S
atur
atio
n Pr
essu
re (p
si)
Time (min)
5 min tissue 20 min 60 min 240 min
R=1.4R=1.6
R=1.0
at 100 ft. depth at surface
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
0
2
4
6
8
10
12
0 20 40 60 80 100 120 140
Tiss
ue S
atur
atio
n Pr
essu
re (p
si)
Time (min)
5 min tissue 20 min 60 min 240 min
Apollo Pre-Launch Decompression
29
R=1.4R=1.6
R=1.0
Transitioning from Earth sea level to 5psi 100% O2
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Solving for Time to Denitrogenate
30
PN2,alveoli = (Pambient − PH2O) fN2
PN2,tissue(t) = PN2,tissue(0) + [(Pambient − PH2O) fN2− PN2,tissue(0)] (1 − e−kt)
e−kt = 1 −PN2,tissue(t) − PN2,tissue(0)
(Pambient − PH2O) fN2 − PN2,tissue(0)
e−kt = 1 −
PN2,tissue
Pambient(t) −
PN2,tissue
Pambient(0)
(1 −PH2O
Pambient ) fN2 −PN2,tissue
Pambient(0)
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Time to Reach Denitrogenation
31
PN2,tissue
Pambient(t) ≡ R(t)
t = − 10.002888 ln 1 − 1.4 − 2.14
(1 − 0.975 ) 0 − 2.14
= 147 min
t = − 1k
ln 1 − R(t) − R(0)
(1 −PH2O
Pambient ) fN2 − R(0)
For Apollo case, 240 min tissue
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
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)
32
T1/2 =ln (2)
kk =
ln (2)T1/2
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
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)
• Dissolved gas partial pressure Pg=Pamb in equilibrium
• Gas pressure in bubble Pint>Pamb due to γ • All bubbles will eventually diffuse and collapse
33
Pinternal = Pambient + Psurface = Pambient +2�
r
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
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
34
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
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
35
rmin =2�
Pg � pambient
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Historical Data on Cabin Atmospheres
36
from Scheuring et. al., “Risk Assessment of Physiological Effects of Atmospheric Composition and Pressure in Constellation Vehicles” 16th Annual Humans in Space, Beijing, China, May 2007
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Spacecraft Atmosphere Design Space
37
from Scheuring et. al., “Risk Assessment of Physiological Effects of Atmospheric Composition and Pressure in Constellation Vehicles” 16th Annual Humans in Space, Beijing, China, May 2007
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Effect of Pressure and %O2 on Flammability
38
from Hirsch, Williams, and Beeson, “Pressure Effects on Oxygen Concentration Flammability Thresholds of Materials for Aerospace Applications” J. Testing and Evaluation, Oct. 2006
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Atmosphere Design Space with Constraints
39
from Scheuring et. al., “Risk Assessment of Physiological Effects of Atmospheric Composition and Pressure in Constellation Vehicles” 16th Annual Humans in Space, Beijing, China, May 2007
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
0.0#
2.0#
4.0#
6.0#
8.0#
10.0#
12.0#
14.0#
0# 200# 400# 600# 800# 1000# 1200#
Tissue
&Nitrogen
&Pressure&(psi)&
Time&(min)&
5*min#.ssue# 80*min#.ssue# 240*min#.ssue#
EVA Denitrogenation - 14.7 psi Cabin
40
Suit Pressure 4.3 psi 100% O2
Cabin Atmosphere 14.7 psi 21% O2
R Value = 1.4
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
0.0#
1.0#
2.0#
3.0#
4.0#
5.0#
6.0#
0# 200# 400# 600# 800# 1000# 1200#
Tissue
&Nitrogen
&Pressure&(psi)&
Time&(min)&
5+min#/ssue# 80+min#/ssue# 240+min#/ssue#
EVA Denitrogenation - 8.3 psi Cabin
41
Suit Pressure 4.3 psi 100% O2
Cabin Atmosphere 8.3 psi 32% O2
R Value = 1.4
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Constellation Spacecraft Atmospheres
42
from Scheuring et. al., “Risk Assessment of Physiological Effects of Atmospheric Composition and Pressure in Constellation Vehicles” 16th Annual Humans in Space, Beijing, China, May 2007
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Categories of Sensing• Proprioception (internal to body)
– “Self-Sensing” – Vestibular (inertial forces) – Muscle and tendon sensors (extension) – Joint sensors (angle)
• Exteroception (external to body) – Visual – Auditory – Cutaneous
43
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Anatomy of the Ear
44
From James T. Joyner, ed., NOAA Diving Manual, Best Publishing, 2001
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Vestibular System
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1985
45
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Vestibular Sense Organs
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1985
46
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Thresholds of Rotational Perception• Rotational accelerations
– Yaw: 0.14 deg/sec2 – Roll and Pitch: 0.5 deg/sec2
• Mulder’s Constant – Acceleration x excitation time = 2 deg/sec – 5 deg/sec2 x 0.5 sec -> sensed – 10 deg/sec2 x 0.1 sec -> not sensed
• Rotational velocities - minimum perceived rotation rates 1-2 deg/sec (all axes)
47
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Otolith Responses
From Roy DeHart, Fundamentals of Aerospace Medicine, Lea & Febiger, 1985
48
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Thresholds of Translational Perception• ax: 0.006 g • ay: 0.006 g • az: 0.01 g • Apparent change in direction of g vector = 1.5°
49
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Space Motion Sickness• “Space Adaptation Syndrome” • 2/3 of astronauts report some effects • Symptoms
– Primary: stomach discomfort, nausea, vomiting – Secondary: pallor, cold sweats, salivation, depressed
appetite, fatigue • No correlation to susceptibility to motion
sickness • Primary hypothesis: sensory conflict (Treisman’s
Theory)
50
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Progression of Space Motion Sickness
51
From Roy DeHart, Fundamentals of Aerospace Medicine, Williams and Wilkins, 1996
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
SAS Experience of First 34 Shuttle Flights
52
0
24
48
72
96
120
First Flight Subsequent FlightNone Mild Moderate Severe
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
SAS Experience of First 34 Shuttle Flights
53
0.00
0.25
0.50
0.75
1.00
First Flight % Subsequent Flight %
None Mild Moderate Severe
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Space Motion Sickness Countermeasures• Preflight training
– Desensitization – Autogenic feedback training (AFT)
• Pharmaceuticals – Oral - scopolamine/dex-amphetamine (Scopdex) – Transdermal - scopolamine – Intramuscular - promethazine
• Mechanical systems – Pressurized insoles – Load suits – Neck restraints
54
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
1
10
100
1000
10000
0 2 4 6
Rotation Rate (rpm)
Lunar gravityMars gravity0.5*Earth gravity0.75*Earth gravityEarth gravity
Artificial Gravity
€
grotation =ω 2r
55
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Allowable Rotation Rates• Select groups (highly trained, physically fit) can
become acclimated to 7 rpm • 95% of population can tolerate 3 rpm • Sensitive groups (elderly, young, pregnant
women) may have tolerance levels as low as 1 rpm
56
Aerospace Physiology ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
References• R. L. DeHart, ed., Fundamentals of Aerospace
Medicine, Second Edition Williams and Wilkins, 1996 • A. E. Nicogossian, C. L. Huntoon, and S. L. Pool, Space
Physiology and Medicine, Third Edition Lea and Febiger, 1994
• A. E. Nicogossian, S. R. Mohler, O. G. Gazenko, and A. I. Grigoriev, eds., Space Biology and Medicine (Volume III, Book 1: Humans in Spaceflight) American Institute of Aeronautics and Astronautics, 1996
• J. T. Joiner, ed., NOAA Diving Manual: Diving for Science and Technology, Fourth Edition Best Publishing, 2001
57