Reference # |
Title |
Download |
Figure
1-15 |
The Wide Range of Space Mission Applications. |
[Link] |
Table
1-4 |
Major Astronautics Professional Societies. |
[Link] |
Table
1-5 |
Major Professional Journals in Astronautics. |
[Link] |
Table
1-6 |
Representative Regularly-Held Conferences in
Astronautics. |
[Link] |
Table
1web-1 |
Space-related Websites. |
[Link] |
Table
2-2 |
Representative Interplanetary Missions. |
[Link] |
Table
2-3 |
The NASA Great Observatories. |
[Link] |
Figure
8-35 |
(Redirected to Table 8-10) Projection
of a Rectangular FOV as Seen from the Spacecraft onto the Earth. |
[Download] |
Table
8-8 |
Coordinates and Dimensions on the
Celestial Sphere for a 1 deg x 1 deg Pixel. |
[Download] |
Table
8-10 |
Planes or Edges Projected onto the Surface of the Earth |
[Download] |
Table
8-11 |
Summary of Computations for Ground Station Passes for LEO
Circular Orbits. |
[Download] |
Table
8-12 |
Summary of Computations for Ground Station Passes for
Elliptical Orbits. |
[Download] |
Table
8-17 |
Representative Mapping and Pointing Error Budgets. |
[Download] |
Figure
9-15 |
Evolution of an Elliptical Orbit Due to Drag. |
[Download] |
Table
9-3 |
Values of the Circular Velocity and Escape Velocity for
the Earth, Sun, Moon, and Mars. |
[Download] |
Table
9-6 |
Planetary Oppositions and Launch Opportunities. |
[Download] |
Table
9-12 |
Synchronous Orbits for Major Solar System Objects. |
[Download] |
Table
9-13 |
Representative Repeating Ground Track Orbits. |
[Download] |
Table
9-14 |
Inclination for Sun-Synchronous Orbits at Various
Altitudes. |
[Download] |
Table
9-19 |
Drift Rate and Total Delta V Required to
Shift a Geosynchronous Satellite 60 deg in
Longitude. |
[Download] |
Table
9-20 |
Representative Turn Angle and Velocity Change for Fly-by
Missions to the Planets. |
[Download] |
Figure
10-7 |
Histogram of Coverage Over a Day for Ground Stations at
the Same Longitude Shown in Fig. 10-6, but Varying Latitudes. |
[Download] |
Figure
10-10 |
Representative Plot of Earth Coverage as a Function of
Latitude. |
[Download] |
Figure
10-12 |
Coverage from Geostationary Orbit as a Function of
Minimum Elevation Angle. |
[Download] |
Figure
10-14 |
Resolution vs. Altitude at Visible Wavelengths for
Satellites in LEO. |
[Download] |
Figure
10-16 |
Representative Orbit Transfer and De-Orbit Delta V
Requirements. |
[Download] |
Figure
10-17 |
Altitude Maintenance Delta V for a Ballistic Coefficient
of 100 kg/m2. |
[Download] |
Figure
10-18 |
Delta V Budget as a Function of Altitude for LEO. |
[Download] |
Figure
10-19 |
Orbit Cost Function for Various Earth Orbiting Missions. |
[Download] |
Figure
10-24 |
(Redirected to Fig. 10-7 and Fig. 10-10)The Repeat
Coverage Orbit. |
[Download] |
Figure
10-25 |
Coverage vs. Latitude for Single Satellites in an RCO and
an SSO. |
[Download] |
Figure
10-35 |
Hohmann Transfer Times, Stay Times, and Round Trip Times for Missions
Between the Earth and Targets at Arbitrary Distances. |
[Download] |
Table
10-3 |
Coverage Formulas for Patterns Shown in Fig. 10-4. |
[Download] |
Table
10-7 |
Creating a Delta V Budget. |
[Download] |
Table
10-14 |
Representative Sun-Synchronous Orbits for Other Central
Bodies. |
[Download] |
Table
10-15 |
Properties of Representative Molniya
Orbits. |
[Download] |
Table
10-16 |
Repeating Ground Track Parameters for Representative
Central Bodies. |
[Download] |
Table
10-31 |
Dimensions of the Sphere of Influences of the Planets in
Our Solar System. |
[Download] |
Table
10-32 |
Summary of the Procedure to Compute the Characteristics
of an Interplanetary Hohmann Transfer. |
[Download] |
Table
10-33 |
Hohmann Transfer Times, Stay Times, and Round Trip Times for
Missions Between the Earth and Neighboring Planets. |
[Download] |
Table
10web-1 |
Summary of the Procedure to Compute the Characteristics
of an Arbitrary Interplanetary Transfer. |
[Download] |
Table
10web-2 |
Summary of the Procedure to Compute the Characteristics
of a Kepler Orbit Connecting Two Arbitrary Points. |
[Download] |
Table
11-8 |
USCM8 Nonrecurring CERs in FY2010 Thousands of Dollars. |
[Download] |
Table
11-9 |
USCM8 Spacecraft Bus Recurring T1 CERs in FY2010 Thousands
of Dollars. |
[Download] |
Table
11-11 |
SSCM Earth Orbiting Total Nonrecurring Cost CERs in
FY2010 Thousands of Dollars. |
[Download] |
Table
11-12 |
QuickCost Nonrecurring Plus Recurring (T1) CER in FY2010 Millions
of Dollars. |
[Download] |
Table
11-14 |
NICM Nonrecurring Hardware Development Plus One Protoflight Unit Cost for Remote Sensing Instrument
Payload in FY2010 Thousands of Dollars. |
[Download] |
Table
11-28 |
Mission Operations Cost Prediction Model. |
[Download] |
Table
11-34 |
FireSat II Space, Ground, and Launch Segment Costs in FY10$K. |
[Download] |
Table
11-35 |
FireSat II Space, Ground, and Launch Segment Costs in FY10$K. |
[Download] |
Table
11-36 |
FireSat II Space, Ground, and Launch Segment Costs in FY10$K. |
[Download] |
Table
11-37 |
SCS Space, Ground, and Launch Segment Costs in FY10$K. |
[Download] |
Table
11-38 |
SCS Space, Ground, and Launch Segment Costs in FY10$K. |
[Download] |
Table
11-39 |
SCS Space, Ground, and Launch Segment Costs in FY10$K. |
[Download] |
Table
13-17 |
Space Principal Alternatives to a Dedicated Launch to
Orbit.. |
[Link] |
Figure
14-5 |
Beta Angle Over a Year for a 400 km, 70 deg Inclination. |
[Download] |
Figure
14-23 |
Eclipse Duration vs. Date for SCS
Spacecraft Over One Year. |
[Download] |
Figure
14-24 |
FireSat II Solar Beta Angle Over a Year of Operations. |
[Download] |
Table
14-19 |
LRO Fuel Budget at Launch. |
[Download] |
Figure
15-3 |
Planck's Blackbody Radiation Curves as a Function of
Wavelength and Frequency. |
[Download] |
Figure
16-10 |
Gain vs. Aperture Diameter, Plotted for Operating Frequencies
Common to Satellite Communications Systems. |
[Download] |
Figure
16-11 |
Antenna Pattern for a Hypothetical 0.75 m Parabolic
Reflector with Uniform Illumination, and Operated at 14 Ghz. |
[Download] |
Figure
16-12 |
Reduction in Gain Resulting from Pointing Loss, Expressed
as a Function of 3dB Beamwidth. |
Not Available |
Figure
16-13 |
Absolute Value of Gain Slope vs. Boresight Angle for the
Antenna Whose Pattern is Presented in Fig. 16-11. |
Not Available |
Figure
16-14 |
Directivity Estimated on the Basis of Coverage Area for Several
Values of Antenna Efficiency. |
[Download] |
Figure
16-16 |
Predicted BER Curves as a Function of
Eb/No. |
[Download] |
Figure
16-17 |
Predicted BER as a Function of
Eb/No. |
[Download] |
Figure
16-18 |
Total Attenuation of Electromagnetic Radiation Versus
Frequency Due to Atmospheric Gases, for a Vertical Path from Sea Level to the
Top of the Atmosphere. |
Not Available |
Table
16-13 |
Sample FSS Link Budget, Forward Direction. |
[Download] |
Table
16web-2 |
Return Link Budget: Use of Earth Coverage Satellite Antenna
Requires Fixed Terminals for Users to Close Link. |
[Download] |
Table
16web-3 |
Forward Link Budget: Use of Earth Coverage Satellite
Antennas Requires Fixed Terminals for Users to Close Link. |
[Download] |
Table
16web-4 |
Return Link Budget: Comparison of Cases for Handheld
Users. |
[Download] |
Table
16web-5 |
Forward Link Budget: Comparison of Cases for Handheld
Users. |
[Download] |
Table
16web-6 |
Intersatellite Link Budget, Ka-Band. |
[Download] |
Table
16web-8 |
Intersatellite Link Budget, Ka-Band. |
[Download] |
Table
17-5 |
Diffraction-Limited Resolution. |
[Download] |
Table
17-9 |
Parameter Calculations for a Passive Optical Sensor. |
[Download] |
Figure
18-3 |
Delta V as a Function of
Mp/Mf and Isp. |
[Download] |
Table
19-16 |
ADCS Vendors. |
[Link] |
Figure
22-15 |
Heat Energy Radiated from a Perfect Emitting Surface
(Black Body) as a Function of the Surface Temperature. |
[Download] |
Figure
22-16 |
Temperature of a Flat Plate Normal to the Sun at 1 AU with
an Insulated Back as a Function of the Surface Properties. |
[Download] |
Table
25-3 |
Representative CubeSat Missions Flown from
2003–2011. |
[Link] |
Table
26-7 |
Summary of Available Launch Vehicles. |
[Link] |
Table
27-1 |
Launch Site Locations and Possible Inclinations (See Isakowitz, et al. [2004] and Strom [2006]. |
[Link] |
Table
I-1 |
Earth Satellite Parameters. |
[Download] |
Reference # |
Title |
Download |
Section
2 Space Mission Communities |
Color photographs in Chapter 2 |
[Link] |
Section
6.5 System Engineering Tools |
Complex Tool Sets |
[Download] |
Section
6.6 The Role of Standards in Space Systems Development |
CCSDS "Recommendation for Space Data System
Standards: Attitude Data Messages" |
[Download] |
Section
9.2 Orbits of the Moon and Planets |
Planetary Configurations |
[Download] |
Section
10.2 Orbit Performance |
Coverage Analysis Example |
[Download] |
Section
10.7 Design of Interplanetary Orbits |
Faster Trajectories |
[Download] |
Section
13.5 Principal Methods for Reducing Cost and Schedule |
Bibliography of Reducing Space Mission Cost |
[Download] |
Section
16.1 Space Mission Communications Architectures |
Figure 16-2. Radio Spectrum Frequency Allocations, as
Defined by the United States National Telecommunications and Information
Administration (NTIA), Showing the Detailed and Complex Assignments of
Bandwidth Across Applications. |
[Download] |
Section
16.4 Sample Missions |
Communications Payload Analysis for SCS and FireSat II
Missions |
[Download] |
Section
17.1 Observation Payload Design |
Complete web article |
[Download] |
Section
17.4 The Evolution of Observation Payloads |
Complete web article |
[Download] |
Section
18.1 Basic Rocket Equations |
Basic Rocket Equations with Varying
Inputs |
[Download] |
Section
18.7 Alternative Propulsions Systems for In-Space Use |
Solar Sail |
[Download] |
Section
18.7 Alternative Propulsions Systems for In-Space Use |
Stationary Polar Orbits discussion and sample
calculations |
[Download] |
Section
18.7.2 Alternative Propulsions Systems for In-Space Use |
Levitated Orbits |
[Download] |
Section
18.8 Examples |
Examples |
[Download] |
Section
19.2 Space Mission Verification and Validation |
Table 19web-1. Typical Onboard Relative Navigation
Sensors |
[Download] |
Section
22.1 Spacecraft Subsystems V—Structures and Thermal |
Spacecraft Structures and Mechanisms |
[Download] |
Section 23.1 LEO Communications Constellations |
Historical Approaches |
[Download] |
Section
23.2 LEO Monolithic vs Distributed Architectures |
DARPA F6 Write-up to be supplied by DARPA |
Not Available |
Section
23.4 System Mission Verification and Validation |
Environmental Testing and Defect Screening |
[Download] |
Section
23.5 Multi-Spacecraft Manufacturing |
Multi-Spacecraft Manufacturing |
[Download] |
Section
25.3 SmallSats |
SmallSat Mission Examples |
[Download] |
Section
26.4 Launch Environments |
Coupled Loads |
[Download] |
Section
26.5 Available Vehicles |
Available Launch Vehicles |
[Download] |
Section
29.1 Mission Planning and Operations Development |
Mission Planning and Operations Development |
[Download] |
Appendix
B. Physical and Orbit Properties of the Sun, Earth, Moon, and Planets |
Complete web article |
[Download] |
Appendix
C |
Orbits about other celestial bodies |
[Download] |
Appendix
C |
Equations Sources |
[Link] |
Appendix
E Time and Date Systems |
Complete web article |
[Download] |
Section
F.2 Vector, Matrix, & Quaternion Algebra |
Matrix and Vector Algebra |
[Download] |
Section
F.2 Vector, Matrix, & Quaternion Algebra |
Quaternions |
[Download] |
Appendix
G Statistical Errors |
Complete web article |
[Download] |