Solar System Tight
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Low-Energy Lunar Trajectory Design
LOW-ENERGY LUNAR TRAJECTORY DESIGN Jeffrey S. Parker and Rodney L. Anderson Jet Propulsion Laboratory Pasadena, California July 2013 ii DEEP SPACE COMMUNICATIONS AND NAVIGATION SERIES Issued by the Deep Space Communications and Navigation Systems Center of Excellence Jet Propulsion Laboratory California Institute of Technology Joseph H. Yuen, Editor-in-Chief Published Titles in this Series Radiometric Tracking Techniques for Deep-Space Navigation Catherine L. Thornton and James S. Border Formulation for Observed and Computed Values of Deep Space Network Data Types for Navigation Theodore D. Moyer Bandwidth-Efficient Digital Modulation with Application to Deep-Space Communication Marvin K. Simon Large Antennas of the Deep Space Network William A. Imbriale Antenna Arraying Techniques in the Deep Space Network David H. Rogstad, Alexander Mileant, and Timothy T. Pham Radio Occultations Using Earth Satellites: A Wave Theory Treatment William G. Melbourne Deep Space Optical Communications Hamid Hemmati, Editor Spaceborne Antennas for Planetary Exploration William A. Imbriale, Editor Autonomous Software-Defined Radio Receivers for Deep Space Applications Jon Hamkins and Marvin K. Simon, Editors Low-Noise Systems in the Deep Space Network Macgregor S. Reid, Editor Coupled-Oscillator Based Active-Array Antennas Ronald J. Pogorzelski and Apostolos Georgiadis Low-Energy Lunar Trajectory Design Jeffrey S. Parker and Rodney L. Anderson LOW-ENERGY LUNAR TRAJECTORY DESIGN Jeffrey S. Parker and Rodney L. Anderson Jet Propulsion Laboratory Pasadena, California July 2013 iv Low-Energy Lunar Trajectory Design July 2013 Jeffrey Parker: I dedicate the majority of this book to my wife Jen, my best friend and greatest support throughout the development of this book and always. -
Ice& Stone 2020
Ice & Stone 2020 WEEK 34: AUGUST 16-22 Presented by The Earthrise Institute # 34 Authored by Alan Hale This week in history AUGUST 16 17 18 19 20 21 22 AUGUST 16, 1898: DeLisle Stewart at Harvard College Observatory’s Boyden Station in Arequipa, Peru, takes photographs on which Saturn’s outer moon Phoebe is discovered, although the images of Phoebe were not noticed until the following March by William Pickering. Phoebe was the first planetary moon to be discovered via photography, and it and other small planetary moons are discussed in last week’s “Special Topics” presentation. AUGUST 16, 2009: A team of scientists led by Jamie Elsila of the Goddard Space Flight Center in Maryland announces that they have detected the presence of the amino acid glycine in coma samples of Comet 81P/ Wild 2 that were returned to Earth by the Stardust mission 3½ years earlier. Glycine is utilized by life here on Earth, and the presence of it and other organic substances in the solar system’s “small bodies” is discussed in this week’s “Special Topics” presentation. AUGUST 16 17 18 19 20 21 22 AUGUST 17, 1877: Asaph Hall at the U.S. Naval Observatory in Washington, D.C. discovers Mars’ larger, inner moon, Phobos. Mars’ two moons, and the various small moons of the outer planets, are the subject of last week’s “Special Topics” presentation. AUGUST 17, 1989: In its monthly batch of Minor Planet Circulars (MPCs), the IAU’s Minor Planet Center issues MPC 14938, which formally numbers asteroid (4151), later named “Alanhale.” I have used this asteroid as an illustrative example throughout “Ice and Stone 2020” “Special Topics” presentations. -
China's Touch on the Moon
commentary China’s touch on the Moon Long Xiao As well as being a milestone in technology, the Chang’e lunar exploration programme establishes China as a contributor to space science. With much still to learn about the Moon, fieldwork beyond Earth’s orbit must be an international effort. hen China’s Chang’e 3 spacecraft geological history of the landing site. touched down on the lunar High-resolution images have shown rocky Wsurface on 14 December 2013, terrain with outcrops of porphyritic basalt, it was the first soft landing on the Moon such as Loong Rock (Fig. 2). Analysis since the Soviet Union’s Luna 24 mission of data collected by the penetrating in 1976. Following on from the decades- Chang’e 3 radar should lead to identification of the old triumphs of the Luna missions and underlying layers of regolith, impact breccia NASA’s Apollo programme, the Chang’e and basalt. lunar exploration programme is leading the China’s robotic field geologist Yutu has charge of a new generation of exploration Basalt outcrop Yutu rover stalled in its traverse of the lunar surface, on the lunar surface. Much like the earlier but plans for the Chang’e 5 sample-return space programmes, the China National mission are moving forward. The primary Space Administration (CNSA) has been objective of the mission will be to return developing its capabilities and technologies 100 m 2 kg of samples from the surface and depths step by step in a series of Chang’e missions UNIVERSITY STATE © NASA/GSFC/ARIZONA of up to 2 m, probably also in the relatively of increasing ambition: orbiting and Figure 1 | The Chinese Chang’e 3 spacecraft and smooth northern Mare Imbrium. -
Information Summaries
TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
Lunar Ionosphere Exploration Method Using Auroral Kilometric Radiation
Earth Planets Space, 63, 47–56, 2011 Lunar ionosphere exploration method using auroral kilometric radiation Yoshitaka Goto1, Takamasa Fujimoto1, Yoshiya Kasahara1, Atsushi Kumamoto2, and Takayuki Ono2 1Kanazawa University, Kanazawa, Japan 2Tohoku University, Sendai, Japan (Received June 3, 2009; Revised November 10, 2010; Accepted January 14, 2011; Online published February 21, 2011) The evidence of a lunar ionosphere provided by radio occultation experiments performed by the Soviet spacecraft Luna 19 and 22 has been controversial for the past three decades because the observed large density is difficult to explain theoretically without magnetic shielding from the solar wind. The KAGUYA mission provided an opportunity to investigate the lunar ionosphere with another method. The natural plasma wave receiver (NPW) and waveform capture (WFC) instruments, which are subsystems of the lunar radar sounder (LRS) on board the lunar orbiter KAGUYA, frequently observe auroral kilometric radiation (AKR) propagating from the Earth. The dynamic spectra of the AKR sometimes exhibit a clear interference pattern that is caused by phase differences between direct waves and waves reflected on a lunar surface or a lunar ionosphere if it exists. It was hypothesized that the electron density profiles above the lunar surface could be evaluated by comparing the observed interference pattern with the theoretical interference patterns constructed from the profiles with ray tracing. This method provides a new approach to examining the lunar ionosphere that does not involve the conventional radio occultation technique. Key words: KAGUYA, lunar ionosphere, auroral kilometric radiation. 1. Introduction 2001; Kurata et al., 2005). The dense plasma layers may The lunar atmosphere is extremely tenuous compared to be maintained by these strong fields. -
Exploration of the Moon
Exploration of the Moon The physical exploration of the Moon began when Luna 2, a space probe launched by the Soviet Union, made an impact on the surface of the Moon on September 14, 1959. Prior to that the only available means of exploration had been observation from Earth. The invention of the optical telescope brought about the first leap in the quality of lunar observations. Galileo Galilei is generally credited as the first person to use a telescope for astronomical purposes; having made his own telescope in 1609, the mountains and craters on the lunar surface were among his first observations using it. NASA's Apollo program was the first, and to date only, mission to successfully land humans on the Moon, which it did six times. The first landing took place in 1969, when astronauts placed scientific instruments and returnedlunar samples to Earth. Apollo 12 Lunar Module Intrepid prepares to descend towards the surface of the Moon. NASA photo. Contents Early history Space race Recent exploration Plans Past and future lunar missions See also References External links Early history The ancient Greek philosopher Anaxagoras (d. 428 BC) reasoned that the Sun and Moon were both giant spherical rocks, and that the latter reflected the light of the former. His non-religious view of the heavens was one cause for his imprisonment and eventual exile.[1] In his little book On the Face in the Moon's Orb, Plutarch suggested that the Moon had deep recesses in which the light of the Sun did not reach and that the spots are nothing but the shadows of rivers or deep chasms. -
Misiones Espaciales Misiones Que Año Nación Lanzador Síntesis De La Misión Recorrido Lo Visitaron
Una vez finalizada la Segunda Guerra Mundial, Estados Unidos y la Unión Soviética se enfrentaron ideológica y políticamente. El campo de batalla de los dos bloques fue llamado Guerra fría. Las dos super potencias se embarcaron en una carrera por la conquista del espacio en un despliegue de poderío científico, militar y tecnológico. En un comienzo los mayores éxitos fueron de la URSS pero fue EE UU el que logró llevar seres humanos a la Luna. Luego de ese suceso, pasaron varios años hasta que otros países lograron el sueño de llegar a nuestro satélite. LMiUNsiones espacAiales En la actual carrera espacial ingresan nuevos proyectos financiados de manera privada. Las misiones que tuvieron éxito en llegar a la Luna se pueden dividir en: las que sobrevolaron, las que orbitaron, las que descendieron con robots y las que lograron llevar humanos Sobrevuelos/Orbitadores: Luna | Ranger | Zond| Lunar Orbiter | Explorer | Clementine | Lunar prospector | Smart | Kaguya Selene|Chang`e| Chandrayaan| Lunar reconnaissance|Grail| Ladee Landers y Rovers: Luna 9| Surveyour|Luna13|Luna 16/20/24| Luna 17|Lunakhod|Yutu Misiones tripuladas: Apollo 8/10/11/12/14/15/16/17 Fuente: http://mars.jpl.nasa.gov/programmissions/missions/ Planetario de Buenos AiresPlanetario de la Ciudad de Buenos Aires Galileo Galilei - Av. Sarmiento y B. Roldán - Tel. 4772-9265 / 4771-6629 - e-mail: [email protected] 1/6 Misiones espaciales Misiones que año Nación Lanzador Síntesis de la misión Recorrido lo visitaron Objetivo: Impactar Sobrevoló la Luna. Luego ingresó en órbita al Sol R-7 Logros : Fue el primer vehículo en escapar de la gravedad Enero Unión terrestre. -
![Arxiv:1912.04482V1 [Physics.Space-Ph] 10 Dec 2019](https://docslib.b-cdn.net/cover/4299/arxiv-1912-04482v1-physics-space-ph-10-dec-2019-744299.webp)
Arxiv:1912.04482V1 [Physics.Space-Ph] 10 Dec 2019
manuscript submitted to Radio Science Measuring the Earth's Synchrotron Emission from Radiation Belts with a Lunar Near Side Radio Array Alexander Hegedus1, Quentin Nenon2, Antoine Brunet3, Justin Kasper1, Ang´elicaSicard3, Baptiste Cecconi4, Robert MacDowall5, Daniel Baker6 1University of Michigan, Department of Climate and Space Sciences and Engineering, Ann Arbor, Michigan, USA 2Space Sciences Laboratory, University of California, Berkeley, CA, USA 3ONERA / DPHY, Universit´ede Toulouse, F-31055 Toulouse France 4LESIA, Observatoire de Paris, Universit PSL, CNRS, Sorbonne Universit, Univ. de Paris, Meudon, France 5NASA Goddard Space Flight Center, Greenbelt, MD, USA 6University of Colorado Boulder, Laboratory for Atmospheric and Space Physics, Boulder, Colorado, USA Key Points: • Synchrotron emission between 500-1000 kHz has a total flux density of 1.4-2 Jy at lunar distances • A 10 km radio array with 16000 elements could detect the emission in 12-24 hours with moderate noise • Changing electron density can make detections 10x faster at lunar night, 10x slower at lunar noon arXiv:1912.04482v1 [physics.space-ph] 10 Dec 2019 Corresponding author: Alexander Hegedus, [email protected] {1{ manuscript submitted to Radio Science Abstract The high kinetic energy electrons that populate the Earth's radiation belts emit synchrotron emissions because of their interaction with the planetary magnetic field. A lunar near side array would be uniquely positioned to image this emission and provide a near real time measure of how the Earth's radiation belts are responding to the current solar in- put. The Salammb^ocode is a physical model of the dynamics of the three-dimensional phase-space electron densities in the radiation belts, allowing the prediction of 1 keV to 100 MeV electron distributions trapped in the belts. -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Dsc Pub Edited
1968 93) few craters, much like the mare sites, Surveyor 7 although the general area was rougher. About Nation: U.S. (43) 21 hours after landing, ground controllers Objective(s): lunar soft-landing fired a pyrotechnic charge to drop the alpha- Spacecraft: Surveyor-G scattering instrument on the lunar surface. Spacecraft Mass: 1,040.1 kg When the instrument failed to move, con- Mission Design and Management: NASA JPL trollers used the robot arm to force it down. Launch Vehicle: Atlas-Centaur (AC-15 / Atlas The scoop on the arm was used numerous 3C no. 5903C / Centaur D-1A) times for picking up soil, digging trenches, Launch Date and Time: 7 January 1968 / and conducting at least sixteen surface- 06:30:00 UT bearing tests. Apart from taking 21,274 pho- Launch Site: ETR / launch complex 36A tographs (many of them in stereo), Surveyor Scientific Instruments: 7 also served as a target for Earth-based 1) imaging system lasers (of 1-watt power) to accurately 2) alpha-scattering instrument measure the distance between Earth and the 3) surface sampler Moon. Although it was successfully reacti- 4) footpad magnet vated after the lunar night, Surveyor 7 Results: Since Surveyors 1, 3, 5, and 6 success- finally shut down on 21 February 1968. In fully fulfilled requirements in support of total, the five successful Surveyors returned Apollo, NASA opted to use the last remaining more than 87,000 photos of the lunar surface Surveyor for a purely scientific mission out- and demonstrated the feasibility of soft- side of exploring a potential landing site for landing a spacecraft on the lunar surface. -
Apollo Over the Moon: a View from Orbit (Nasa Sp-362)
chl APOLLO OVER THE MOON: A VIEW FROM ORBIT (NASA SP-362) Chapter 1 - Introduction Harold Masursky, Farouk El-Baz, Frederick J. Doyle, and Leon J. Kosofsky [For a high resolution picture- click here] Objectives [1] Photography of the lunar surface was considered an important goal of the Apollo program by the National Aeronautics and Space Administration. The important objectives of Apollo photography were (1) to gather data pertaining to the topography and specific landmarks along the approach paths to the early Apollo landing sites; (2) to obtain high-resolution photographs of the landing sites and surrounding areas to plan lunar surface exploration, and to provide a basis for extrapolating the concentrated observations at the landing sites to nearby areas; and (3) to obtain photographs suitable for regional studies of the lunar geologic environment and the processes that act upon it. Through study of the photographs and all other arrays of information gathered by the Apollo and earlier lunar programs, we may develop an understanding of the evolution of the lunar crust. In this introductory chapter we describe how the Apollo photographic systems were selected and used; how the photographic mission plans were formulated and conducted; how part of the great mass of data is being analyzed and published; and, finally, we describe some of the scientific results. Historically most lunar atlases have used photointerpretive techniques to discuss the possible origins of the Moon's crust and its surface features. The ideas presented in this volume also rely on photointerpretation. However, many ideas are substantiated or expanded by information obtained from the huge arrays of supporting data gathered by Earth-based and orbital sensors, from experiments deployed on the lunar surface, and from studies made of the returned samples. -
(Est Pub Date) Sid: Preliminary Analysis of Luna 9
Directorate of Science and Technology [b)[1J TOP SECReT [b)[3J CONTENTS Preliminary Analysis of Luna 9 . • . TOP SBGRET ''OP 8BCRET PRELIMINARY ANALYSIS OF LUNA 9 SUMMARY AND CONCLUSIONS The success of Luna 9 in soft-landing on the moon and transmitting data back to the earth represents a significant accomplishment in the Soviet lunar ex ploration program. The numerous un successful efforts that preceded Luna 9 indicate the high priority placed on a lunar landing by the USSR. Information derived from Luna 9 is valuable to both the United States and In addition, the Soviets said that Luna 9 the Soviet Union. Luna 9 proved that made radiation measurements and found a vehicle can be successfully softlanded that the radiation level on the moon is on the moon. This in turn, may lead to well within the acceptable limits for some optimism regarding future manned human beings. The Luna 9 payload lunar landings. appears to be of relatively simple design using subsystems of minimum com plexity consistent with achieving its mis sions. Mar 66 - 1 - TOP 8ECRET DISCUSSION Previous Launch AttemPts teries were contained inside the sphere. The station was said to be about two feet Luna 9 was the twelfth attempted lunar above the lunar surface, but it is not clear mission* in a program dating back to whether this figure refers to the diameter January 1963. Of the previous 11 at of the sphere or to the height ofthe photo tempts, four failed while in their park facsimile viewing device above the sur ing orbit, two failed during ejection from face.