Presentation is loading. Please wait.

Presentation is loading. Please wait.

1.

Similar presentations


Presentation on theme: "1."— Presentation transcript:

1 1

2 2

3 3

4 4

5 5

6 Ways of Addressing Radiation Risks
General Options Surface Options In-space Options 7

7 Ways of Addressing Radiation Risks
General Options: Accept the risks Astronaut selection Medications e.g. RLIP 76 8

8 Ways of Addressing Radiation Risks
Surface Options: Cover habitat with regolith Limit EVAs 10

9 Ways of Addressing Radiation Risks
In-space Options: Positioning supplies & equipment Positioning propellant Water / ice Smart shielding material Magnetic fields Electrostatic shielding 9

10 Surface Options – Covering with Regolith
11

11 14

12 Source: Bigelow Aerospace
Source: Univ. of Maine 12

13 Source: TripAdvisor.com
Source: laughingsquid.com Source: wallmuralsgallery.com Source: laughingsquid.com

14 In-space Options – Hollow Sphere Shielding
[Regarding solar electric propulsion to Mars] We can do fast dashes from place to place but there is a lot of work to do to get there. Or it [the radiation issue] may be sufficiently serious that even fast dashes won’t deal with it, but fortunately Buzz Aldrin solved that problem too, and you do that by putting cycler habs up and you shield the heck out of them and then you take the cruise line to Mars instead of taking your sprint”. 16

15 19

16 19

17 Internal Diameter Thickness Launcher Mission Duration Risk

18 Internal Diameter

19

20

21 Internal Diameter SkyLab 6.7 meters

22 Launcher

23 6

24 (1.5% of NASA’s annual budget)
26

25 2 Falcon Heavies 80.9 metric tonnes Launcher

26 Thickness

27 Thickness Thickness = 50 cm

28 Thickness 51.6 cm

29 Mission Duration Inspiration Mars 589 Days

30 Risk

31 Blood Forming Organ (BFO) dose equivalent, rem/yr
Aluminum Water Hydrogen 51.6 Shield thickness, g/cm Figure 6. Shielding effectiveness of GCR at solar minimum 23

32

33 6

34 220 mSv / mission 38% of career limit Risk

35 20

36 21 1% Mars atmosphere 5% Suggested shielding protection 24%
30,000 ft (Commercial airplanes) 50% 18,000 ft 54% 16,728 ft (La Rinconada - Highest town in the world) 83% 5280 ft (Denver) 21 100% 0 ft

37 1,063 cm 51.6 cm 22

38 Blood Forming Organ (BFO) dose equivalent, rem/yr
Aluminum Water Hydrogen 51.6 Shield thickness, g/cm Figure 6. Shielding effectiveness of GCR at solar minimum 23

39 Blood Forming Organ (BFO) dose equivalent, rem/yr
Aluminum Water Hydrogen 6.7 Shield thickness, g/cm Figure 6. Shielding effectiveness of GCR at solar minimum 24

40 Ways of Addressing Radiation Risks
51.6 cm 6.7 m 80 mT 25

41 27

42

43 Sphere within sphere Solar panels Water Xe Air Inflatable hab

44

45

46

47

48 Air Air

49

50

51

52

53

54

55

56

57

58

59

60

61

62

63

64

65 Hollow ice sphere

66

67

68

69

70

71

72

73

74

75

76

77

78

79

80

81

82

83

84

85 98

86 2 years later while passing Earth
99

87

88

89

90

91

92

93

94

95

96

97

98

99

100

101

102

103

104

105

106

107

108

109

110

111

112

113

114

115

116

117

118

119

120

121

122

123

124

125

126

127

128

129

130

131

132

133

134

135

136

137

138

139

140

141

142

143

144

145

146

147

148

149

150 Mild artificial gravity
Launch once Use many times Spacious Radiation protection Mild artificial gravity 163

151 164

152 165

153 166

154 167

155 168

156 169

157 170

158 171

159 172

160 173

161 174

162 175

163 176

164 177

165

166 15


Download ppt "1."

Similar presentations


Ads by Google