LIST OF ILLUSTRATIONS
Chapters
Page
2. Space Environment:
Figure 1. The solar system
11
3. Trajectories and Orbits:
Figure 1. Types of paths
20
Figure 2. Interplanetary trajectories
22
Figure 3. Velocity requirements for ballistic missile and space flight
24
4. Rocket Vehicles:
Figure 1. Velocity characteristics of rocket vehicles
29
Figure 2. Rocket vehicle characteristics
30
5. Propulsion Systems:
Figure 1. Schematic of solid-propellant rocket
32
Figure 2. Schematic of liquid-propellant rocket
33
Figure 3. Nuclear rocket
35
Figure 4. Solar sail
37
Figure 5. Ion rocket engine
38
Figure 6. Plasma jet
39
7. Internal Power Sources:
Figure 1. Solar-powered alternator unit
50
Figure 2. Utilization of isotope power
52
Figure 3. Promethium battery
53
8. Structures and Materials:
Figure 1. Sheet stringer construction
56
Figure 2. Waffle construction
57
Figure 3. Typical sandwich panel with hexagonal cell core
57
9. Flight Path and Orientation Control:
Figure 1. Jet-vane control
61
Figure 2. Control by rotating mass
63
13. Atmospheric Flight:
Figure 1. Glide path
86
Figure 2. Typical glide rocket
87
Figure 3. Various types of atmospheric entry
89
Figure 4. Approach paths from space
90
Figure 5. Aerodynamic braking, shift from a parabolic approach orbit to a satellite orbit
91
Figure 6. Aerodynamic forces on various bodies
92
Figure 7. Density distribution in planetary atmospheres
93
Figure 8. A simple analogy
95
Figure 9. Velocity and deceleration during direct entry into the Earth's atmosphere from space at various angles
96
Figure 10. Velocity and deceleration during direct entry from space at
=90° into three planetary atmospheres
97
14. Landing and Recovery:
Figure 1. Impact vehicle with penetration spike
103
Figure 2. Rough landing instrument carrier
103
Figure 3. Soft landing vehicle
103
Figure 4. Soft landing vehicle, full assembly
104
15. Environment of Manned Systems:
Figure 1. Stress-time effects on humans
107
Figure 2. Human time-tolerances-oxygen partial pressure
109
Figure 3. Human tolerances-atmospheric composition and pressure
111
Figure 4. Human time-tolerance-carbon dioxide partial pressure
112
Figure 5. Human time-tolerance-acceleration
115
Figure 6. Approximate human time-tolerances Temperature
117
251
252 ASTRONAUTICS AND ITS APPLICATIONS
LIST OF ILLUSTRATIONS-Continued
Chapters
15. Environment of Manned Systems-Continued:
Page
Figure 7. Effect of temperature on water, food, and oxygen requirements
119
Figure 8. Human tolerances to radiation
121
Figure 9. Production of X-rays inside space vehicle due to Bremsstrahlung caused by protons and electrons
122
17. Nuclear Weapon Effects in Space:
Figure 1. Weapon effects at surface (20 KT)
132
Figure 2. Nuclear radiation intensities (20 KT)
133
20. Specific Flight Possibilities:
Figure 1. Ballistic missile range
146
Figure 2. Velocity requirements for sounding rockets and satellites
147
Figure 3. Typical satellite ascent trajectory
148
Figure 4. Earth satellite velocity and period versus orbital altitude
149
Figure 5. "Kick-in-the-apogee" technique of satellite launching
151
Figure 6. Recoverable satellite ejection and reentry velocities
152
Figure 7. Satellite recovery parameters
153
Figure 8 Moon-rocket transit trajectory-impact
154
Figure 9 Moon-rocket trajectory as seen from the Moon
155
Figure 10. Effect of varying velocity on impact location
155
Figure 11. Initial conditions for lunar impact
156
Figure 12. Total velocity and path angle tolerances to hit the Moon
158
Figure 13. Transit time from Earth to Moon
159
Figure 14. Return near Earth after passing near the Moon-returning vehicle moving in same direction as Earth's rotation
160
Figure 15. Return near the Earth after passing near the Moon- returning vehicle moving in direction opposite from Earth's rotation
161
Figure 16. Transit trajectory-escape from the Earth
162
Figure 17. Transit trajectory-lunar satellite
163
Figure 18. Moon satellite orbit
164
Figure 19. Relative positions of libration centers in the Earth- Moon system
165
Figure 20. Flights to Venus in various positions
169
Figure 21. Velocity penalty for launching after most favorable dates
170
21. Observation Satellite:
Figure 1. Photograph
176
Figure 2. Analysis of photograph (fig. 1)
177
Figure 3. Photograph
179
Figure 4. Lunar photography and aerial photography: Resolution comparison
186
Figure 5. Viewing an area on the Earth at 45° latitude from the "24 hour" satellite
187
Figure 6. Required focal length variation with altitude for ground resolutions of 1, 4, 20, and 100 feet assuming a film resolution of 100 lines per millimeter
189
22. Meteorological Satellites:
Figure 1. Photograph
194
26. Bombing from Satellites:
Figure 1. Bomb delivery from a satellite
208
27. Scientific Space Exploration:
Figure 1. The radiation spectrum
210
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