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ویرایش:
نویسندگان: Thomas Lund
سری: Springer Praxis Books
ISBN (شابک) : 3031298373, 9783031298370
ناشر: Springer-Praxis
سال نشر: 2023
تعداد صفحات: 366
زبان: English
فرمت فایل : PDF (درصورت درخواست کاربر به PDF، EPUB یا AZW3 تبدیل می شود)
حجم فایل: 17 Mb
در صورت تبدیل فایل کتاب Spacecraft that Explored the Inner Planets Venus and Mercury به فرمت های PDF، EPUB، AZW3، MOBI و یا DJVU می توانید به پشتیبان اطلاع دهید تا فایل مورد نظر را تبدیل نمایند.
توجه داشته باشید کتاب فضاپیما که در مورد سیارات داخلی زهره و جیوه کاوش کرده است نسخه زبان اصلی می باشد و کتاب ترجمه شده به فارسی نمی باشد. وبسایت اینترنشنال لایبرری ارائه دهنده کتاب های زبان اصلی می باشد و هیچ گونه کتاب ترجمه شده یا نوشته شده به فارسی را ارائه نمی دهد.
Introduction Contents Chapter 1: The Planets of the Sun Characteristics of Venus Characteristics of Mercury Bibliography Chapter 2: Launch Vehicles for Planetary Spacecraft Early Soviet Union Space Programs Soviet Union Launch Site for Early Planetary Spacecraft Soviet Union Launch Vehicles for Early Planetary Spacecraft Soyuz-Molniya 8 K78 Lunch Vehicle Molniya 8K78M Launch Vehicle Proton-K Launch Vehicle Early United States Space Programs United States Launch Sites for Early Planetary Spacecraft United States Launch Vehicles for Planetary Spacecraft Atlas-Agena Launch Vehicles Atlas-Centaur Launch Vehicles Titan III/Centaur Launch Vehicles Space Shuttle Launch Vehicle Delta II Launch Vehicle Falcon 9 Launch Vehicle Japanese Launch Vehicle for Akatsuki Spacecraft to Venus Tanegashima Space Center European Space Agency (ESA) Launch Vehicle Soyuz-Fregat Soyuz-FG Launch Vehicle Fregat Upper Stage Bibliography Chapter 3: Soviet Union Spacecraft That Explored Venus 1960–1980 1VA Spacecraft (Sputnik 7 and Venera 1) Flight of the 1VA Spacecraft 2MV Spacecraft 2MV-1 Spacecraft 2MV Bus 2MV-1 Landing Capsule 2MV-2 Spacecraft Flights of the 2MV-1 and 2MV-2 Spacecraft 3MV Spacecraft (Venera 2 and Venera 3) Background of 3MV Spacecraft 3MV-1 Spacecraft 3MV Bus Landing Capsule Repurposed Spacecraft Originally Planned for Mars Flights of the 3MV Spacecraft to Venus V-67 Spacecraft (Venera 4) Design of V-67 Spacecraft Landing Capsule Flights of the V-67 Spacecraft Venera 4 Kosmos 167 V-69 Spacecraft (Venera 5 and Venera 6) Design of V-69 Spacecraft Flight of the V-69 Spacecraft Venera 5 Venera 6 V-70 Spacecraft (Venera 7) Flight of the V-70 Spacecraft Venera 7 Kosmos 359 V-72 Spacecraft (Venera 8) Bus Landing Capsule Flight of V-72 Spacecraft Venera 8 4V-1 Spacecraft (Venera 9 and Venera 10) Bus Obiter Experiments on the Bus 4V-1 Lander Lander Experiments Flight of 4V-1 Spacecraft Venera 9 and Venera 10 Venera 9 Venera 10 Experiments Conducted by the Landers Operation of the Orbiter 4V-1 Spacecraft, Venera 11 and Venera 12 Flights of 4V-1 Spacecraft Venera 11 and Venera 12 Venera 11 Venera 12 Lander Operations Color Cameras Mass Spectrometer Gas Chromatograph (Sigma) X-Ray Fluorescence Spectrometer Low Frequency Radio Sensor (GROZA) Penetrometer (PROP-V) Bus SIGNE 2 Gamma-ray Burst Detector KONUS Gamma-ray Burst Detector Bibliography Chapter 4: U.S. Spacecraft that Explored Venus 1960–1980 Mariner R Spacecraft (Mariner 1 and Mariner 2) Mechanical Configuration Mariner R Systems Spacecraft Power Central Computer and Sequencer Attitude Control System Midcourse Correction Rocket Engine Telecommunications Subsystem Experiments Carried by Mariner 2 Microwave Radiometer Configuration of Microwave Radiometer Infrared Radiometer Magnetometer High Energy Radiation Experiment Solar Plasma Analyzer Cosmic Dust Sensor Flight of Mariner 1 and Mariner 2 Spacecraft Flight of Mariner 1 Flight of Mariner 2 Mariner 5 Spacecraft Background of Mariner 5 Mechanical Configuration of Mariner 5 Mariner 5 Systems Midcourse Correction Rocket Engine Spacecraft Power Guidance and Control Special Sensors Telecommunications Subsystem Command Detector and Decoder Data Encoder Data Automation Subsystem Tape Recorder Subsystem Science Experiments Carried by Mariner 5 Trapped Radiation Detector Solar Plasma Probe Helium Magnetometer Ultraviolet Photometer Dual–Frequency Receiver Flight of Mariner 5 Pioneer Venus Orbiter Background of Pioneer Venus Mission Mechanical Configuration of Pioneer Venus Orbiter Pioneer Venus Orbiter Systems Orbit Insertion Rocket Motor Spacecraft Power Telecommunications Attitude and Maneuvering Control Science Experiments Carried by Pioneer Venus Orbiter Magnetometer Experiment Surface Mapping Radar Orbiter Infrared Radiometer Ultraviolet Spectrometer Cloud Photopolarimeter Gamma Ray Burst Detector Pioneer Venus Multiprobe Mechanical Configuration of Pioneer Venus Multiprobe Multiprobe Bus Systems Power Subsystem Communications Attitude and Maneuvering Control Science Experiments Carried by Multiprobe Bus Neutral Mass Spectrometer Ion Mass Spectrometer Pioneer Venus Large Probe Mechanical Configuration of Large Probe Descent of the Large Probe Large Probe Systems Power Subsystem Communications Subsystem Command Subsystem Data Transmission to Earth Science Experiments Carried by Large Probe Neutral Mass Spectrometer Gas Chromatograph Solar Flux Radiometer Infrared Radiometer Cloud Particle Size Spectrometer (LCPS) Nephelometer (LN/SN) Atmosphere Structure Experiments (LAS/SAS) Pioneer Venus Small Probes Mechanical Configuration of Small Probes Descent of the Small Probes Small Probe Systems Power Subsystem Communications Subsystem Command Subsystem Data Transmission to Earth Science Experiments Carried by the Small Probe Net Flux Radiometer Bibliography Chapter 5: Soviet Union Spacecraft that Explored Venus 1980–1990 4 V-1 Spacecraft (Venera 13 and Venera 14) Flight of Venera 13 and Venera 14 Scientific Experiments on Venera 13 and 14 Landers Color Cameras Mass Spectrometer Gas Chromatograph (Sigma 2) X-Ray Fluorescence Spectrometer Analysis of Clouds X-Ray Fluorescence Spectrometer Analysis of Soil and Rocks Optical Spectrometer Penetrometer (PROP-V) Low Frequency Radio Sensor (GROZA 2) Landing Sites for the Venera Spacecraft 4 V-2 Spacecraft (Venera 15 and Venera 16) Mechanical Configuration of Venera 15 and 16 Flight of Venera 15 and Venera 16 Scientific Experiments on Venera 15 and 16 Synthetic Aperture Radar Radar Altimeter Infrared Spectrometer Cosmic Ray Detector 5VK Spacecraft (Vega 1 and Vega 2) Mechanical Configuration of Vega 1 and Vega 2 Flight of the Vegas Flight of Vega 1 Flight of Vega 2 Experiments on Vega Bus for Exploration of Comet Halley Television System (TVS) Infrared Spectrometer (IKS) Three Channel Spectrometer (TKS) Balloon Borne Exploration of Venus Experiments on the Balloon Data Transmission from Experiments Determination of Venus Winds by Earth-Based Tracking of Balloons Vega Lander Experiments on Vega Landers Ultraviolet Absorption Spectrometer (ISAV-S) Optical Aerosol Analyzer (ISAV-A) Aerosol Particle-Size Counter (LSA) Aerosol Mass Spectrometer (MALAKHIT-M) Hygrometer (VM-4) X-Ray Fluorescence Spectrometer (IFP) Gas Chromatograph (SIGMA-3) Gamma Ray Spectrometer Soil X-Ray Fluorescence Spectrometer (BDRP-AM25) Temperature and Pressure Sensors (METRO) Conclusion Bibliography Chapter 6: U.S. Magellan Spacecraft that Explored Venus 1980–2020 Background of Magellan Program Mechanical Configuration of the Magellan Spacecraft Magellan Systems Propulsion System Attitude Control System Command and Data Subsystem Telecommunications Spacecraft Power Radar Sensor Flight of Magellan Mapping Mission Synthetic Aperture Radar Mapping Radar Altimeter Mapping Radiometric Mapping Gravimetric Mapping Conclusion Bibliography Chapter 7: U.S. Spacecraft that Explored Mercury: Mariner 10 and Messenger Mariner 10 Spacecraft Background of Mariner 10 Mechanical Configuration of Mariner 10 Mariner 10 Systems Trajectory Correction Rocket Motor Attitude Control Subsystem Articulation and Pointing Subsystem Spacecraft Power Central Computer and Sequencer Flight Data Subsystem Telecommunications System Command Decoder Science Experiments Carried by Mariner 10 Television Cameras Infrared Radiometer Ultraviolet Airglow Spectrometer Ultraviolet Occultation Spectrometer Magnetometer Plasma Science Experiment Charged Particles Telescope S-Band and X-Band Radio Occultation Flight of Mariner 10 Conclusion Messenger Spacecraft Background of Messenger Program Mechanical Configuration of the Messenger Spacecraft Messenger Systems Propulsion System Electrical Power Subsystem Attitude Control Guidance and Control Telecommunications Command and Data Handling Flight of Messenger Science Experiments Carried by Messenger Mercury Dual Imaging System (MDIS) Images from Messenger Mission Mercury Atmospheric and Surface Composition Spectrometer (MASCS) Gamma-Ray and Neutron Spectrometer (GRNS) X-Ray Spectrometer (XRS) Magnetometer (MAG) Energetic Particle and Plasma Spectrometer (EPPS) Mercury Laser Altimeter (MLA) Conclusion Mission Patch for the Messenger Program Bibliography Chapter 8: Japanese and European Space Agency Spacecraft that Explored Venus 2005–2020 Venus Express Spacecraft Mechanical Configuration of Venus Express Venus Express Systems Propulsion System Attitude Control Electrical Power for Venus Express Telecommunications System Data Management System Flight of Venus Express Scientific Instruments Venus Monitoring Camera Analyser of Space Plasma and Energetic Atoms (ASPERA-4) Magnetometer (MAG) Planetary Fourier Spectrometer (PFS) Spectroscopy for Investigation of Characteristics of the Atmosphere of Venus/Solar Occultation at Infrared (SPICA/SOIR) Visible and Infrared Thermal Imaging Spectrometer (VIRTIS) Akatsuki Spacecraft (Japan) Mechanical Configuration of Akatsuki Akatsuki Systems Propulsion System Attitude Control Electrical Power Telecommunications System Flight of Akatsuki Science Instruments Ultraviolet Imager (UVI) 1 μm Camera (IR1) 2 μm Camera (IR2) Long-Wave Infrared Camera (LIR) Digital Electronics Unit Lightning and Airglow Camera (LAC) Radio Occultation Experiment Bibliography Index