Voyager to the Outer Planets and Into Interstellar Space
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Stardust Comet Flyby
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Stardust Comet Flyby Press Kit January 2004 Contacts Don Savage Policy/Program Management 202/358-1727 NASA Headquarters, Washington DC Agle Stardust Mission 818/393-9011 Jet Propulsion Laboratory, Pasadena, Calif. Vince Stricherz Science Investigation 206/543-2580 University of Washington, Seattle, WA Contents General Release ……………………………………......………….......................…...…… 3 Media Services Information ……………………….................…………….................……. 5 Quick Facts …………………………………………..................………....…........…....….. 6 Why Stardust?..................…………………………..................………….....………......... 7 Other Comet Missions ....................................................................................... 10 NASA's Discovery Program ............................................................................... 12 Mission Overview …………………………………….................……….....……........…… 15 Spacecraft ………………………………………………..................…..……........……… 25 Science Objectives …………………………………..................……………...…........….. 34 Program/Project Management …………………………...................…..…..………...... 37 1 2 GENERAL RELEASE: NASA COMET HUNTER CLOSING ON QUARRY Having trekked 3.2 billion kilometers (2 billion miles) across cold, radiation-charged and interstellar-dust-swept space in just under five years, NASA's Stardust spacecraft is closing in on the main target of its mission -- a comet flyby. "As the saying goes, 'We are good to go,'" said project manager Tom Duxbury at NASA's Jet -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
Giant Planet / Kuiper Belt Flyby
Giant Planet / Kuiper Belt Flyby Amanda Zangari (SwRI) Tiffany Finley (SwRI) with Cecilia Leung (LPL/SwRI) Simon Porter (SwRI) OPAG: February 23, 2017 Take Away • New Horizons provided scientifically valuable exploration of the Kuiper Belt in the New Frontiers cost cap. • The Kuiper Belt is full of objects with a diverse range of stories that go beyond what we learned from Pluto. • Giant Planet flybys add scientific value to a Kuiper Belt mission • Found preliminary trajectory examples for high interest KBOs-- Haumea, Varuna, 2015 RR245 can be reached via Jupiter AND Saturn, Uranus or Neptune flyby in the 2030s. • To be a candidate New Frontiers mission, a 2 Giant planet+KBO mission must be endorsed by a decadal survey according to current rules. New Horizons Heritage NH Jupiter Encounter planned around Pluto flyby timing, which was dominated by achieving quadruple occultations, “interesting” side up. New Horizons Heritage Pluto flyby took advantage of Ecliptic crossing, enabling access to the cold classical belt (where 2014 MU69 is located). New Horizons Heritage 2014 MU69 discovered while in flight. Targeting was from spacecraft propulsion and took advantage of cold classical population density. Object is small, reddish ~40 km diameter. Saturn’s moons show incredible diversity NASA/JPL As do Uranus and Neptune Some Kuiper Belt Geography Where do we want to go? Getting there- JGA “anytime” New Horizons model: Fast Launch, Jupiter Flyby, Launch window every 11 years McGranaghan et al 2011 Can we go to more than just Jupiter? If so, where, what? New Horizons 2 • 2008 launch using New Horizons flight spares • Proposed Jupiter flyby, equinox flyby of Uranus, and flyby of (47171) 1999 TC36 (now know to be trinary). -
NASA's MESSENGER Sends Flyby Data to Earth Using
Press Release For immediate release Special Delivery: NASA’s MESSENGER Sends Flyby Data to Earth Using CCSDS File Delivery Protocol Developed for Deep Space by International Team WASHINGTON, Aug. 10 (CCSDS) – NASA’s MESSENGER team is using the CCSDS File Delivery Protocol (CFDP), a highly specialized protocol designed to overcome space operations communications challenges, to download data captured during a successful flyby of Earth last week. A team of international space data communications experts, collaborating through the Consultative Committee for Space Data Systems (CCSDS), developed CFDP to reliably and efficiently downlink files from a spacecraft even in the strenuous environment of deep space. Since the MESSENGER spacecraft’s launch a year ago, it has successfully used CFDP to enable mission communications and will use it throughout its 7.9-billion kilometer journey to Mercury. In using CFDP, MESSENGER communications represents a change in the standard method of storing science and housekeeping data on spacecraft built by the Johns Hopkins University Applied Physics Laboratory (JHU/APL). MESSENGER is also the first U.S. space flight mission to use CFDP in mission operations. Prior to MESSENGER, JHU/APL missions used a raw storage model of storing data, but new mission and operational requirements meant that MESSENGER would have to incorporate a file system of data storage into its spacecraft software architecture. A reliable method of downlinking files to the ground had to be found and CFDP was chosen by mission planners to do the job. CFDP is included in the MESSENGER software architecture through a reuse of a NASA Jet Propulsion Lab (NASA JPL) implementation on the ground and a JHU/APL “CFDP-lite” implementation on the flight side. -
Mariner to Mercury, Venus and Mars
NASA Facts National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, CA 91109 Mariner to Mercury, Venus and Mars Between 1962 and late 1973, NASA’s Jet carry a host of scientific instruments. Some of the Propulsion Laboratory designed and built 10 space- instruments, such as cameras, would need to be point- craft named Mariner to explore the inner solar system ed at the target body it was studying. Other instru- -- visiting the planets Venus, Mars and Mercury for ments were non-directional and studied phenomena the first time, and returning to Venus and Mars for such as magnetic fields and charged particles. JPL additional close observations. The final mission in the engineers proposed to make the Mariners “three-axis- series, Mariner 10, flew past Venus before going on to stabilized,” meaning that unlike other space probes encounter Mercury, after which it returned to Mercury they would not spin. for a total of three flybys. The next-to-last, Mariner Each of the Mariner projects was designed to have 9, became the first ever to orbit another planet when two spacecraft launched on separate rockets, in case it rached Mars for about a year of mapping and mea- of difficulties with the nearly untried launch vehicles. surement. Mariner 1, Mariner 3, and Mariner 8 were in fact lost The Mariners were all relatively small robotic during launch, but their backups were successful. No explorers, each launched on an Atlas rocket with Mariners were lost in later flight to their destination either an Agena or Centaur upper-stage booster, and planets or before completing their scientific missions. -
EPOXI COMET ENCOUNTER FACT SHEET Nov
EPOXI COMET ENCOUNTER FACT SHEET Nov. 2, 2010 Quick Facts Flyby Spacecraft Dimensions: 3.3 meters (10.8 feet) long, 1.7 meters (5.6 feet) wide, and 2.3 meters (7.5 feet) high Weight: 601 kilograms (1,325 pounds) at launch, consisting of 517 kilograms (1,140 pounds) spacecraft and 84 kilograms (185 pounds) fuel. On 10/25/10 there was 4 kilograms (8.8 pounds) of fuel remaining. Power: 2.8-meter-by-2.8-meter (9-foot-by-9 foot) solar panel providing up to 750 watts, depending on distance from sun. Power storage via small, 16-amp- hourrechargeable nickel hydrogen battery Comet Hartley 2 Nucleus shape: Elongated Nucleus size (estimated): About 2.2 kilometers (1.4 miles) long Nucleus mass: Roughly 280 million metric tons Nucleus rotation period: About 18 hours Nucleus composition: Water ice, carbon dioxide ice, silicate dust Mission Launch: Jan. 12, 2005 Launch site: Cape Canaveral Air Force Station, Florida Launch vehicle: Delta II 7925 with Star 48 upper stage Impact with Tempel 1: 10:52 p.m. PDT July 3, 2005 (1:52 a.m. EDT July 4, 2005) Earth-comet distance at time of impact: 133.6 million kilometers (83 million miles) Total distance traveled by spacecraft from Earth to Tempel 1: 431 million kilometers (268 million miles) Flyby of Hartley 2: About 10 a.m. EDT or 7 a.m. PDT Nov. 4, 2010 Additional distance traveled by spacecraft to Hartley 2: About 4.6 billion kilometers (2.9 billion miles) Program Cost of Deep Impact: $267 million total (not including launch vehicle), consisting of $252 million spacecraft development and $15 million mission operations Cost of EPOXI extended mission: $42 million, for operations from 2007 to end of project at the end of fiscal year 2011. -
Method for Rapid Interplanetary Trajectory Analysis Using Δv Maps with Flyby Options
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by DSpace@MIT METHOD FOR RAPID INTERPLANETARY TRAJECTORY ANALYSIS USING ΔV MAPS WITH FLYBY OPTIONS TAKUTO ISHIMATSU*, JEFFREY HOFFMAN†, AND OLIVIER DE WECK‡ Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, MA 02139, USA. Email: [email protected]*, [email protected]†, [email protected]‡ This paper develops a convenient tool which is capable of calculating ballistic interplanetary trajectories with planetary flyby options to create exhaustive ΔV contour plots for both direct trajectories without flybys and flyby trajectories in a single chart. The contours of ΔV for a range of departure dates (x-axis) and times of flight (y-axis) serve as a “visual calendar” of launch windows, which are useful for the creation of a long-term transportation schedule for mission planning purposes. For planetary flybys, a simple powered flyby maneuver with a reasonably small velocity impulse at periapsis is allowed to expand the flyby mission windows. The procedure of creating a ΔV contour plot for direct trajectories is a straightforward full-factorial computation with two input variables of departure and arrival dates solving Lambert’s problem for each combination. For flyby trajectories, a “pseudo full-factorial” computation is conducted by decomposing the problem into two separate full-factorial computations. Mars missions including Venus flyby opportunities are used to illustrate the application of this model for the 2020-2040 time frame. The “competitiveness” of launch windows is defined and determined for each launch opportunity. Keywords: Interplanetary trajectory, C3, delta-V, pork-chop plot, launch window, Mars, Venus flyby 1. -
So, Has Voyager 1 Left the Solar System? Scientists Face Off Cosmic-Ray Fluctuations Could Mean the Craft Has Exited the Sun's Magnetic Field
NATURE | NEWS So, has Voyager 1 left the Solar System? Scientists face off Cosmic-ray fluctuations could mean the craft has exited the Sun's magnetic field. Ron Cowen 21 March 2013 A space physicist this week suggests that NASA’s venerable Voyager 1 spacecraft has become the first vehicle to venture beyond the heliosphere — the magnetic bubble created by the Sun — but other mission scientists disagree. William Webber of New Mexico State University in Las Cruces bases the claim on signals recorded last August by the Voyager 1 cosmic-ray subsystem — a device that he helped to build — along with his late colleague and study co-author Francis McDonald. JPL-Caltech/NASA Voyager 1 recorded a sudden drop in cosmic rays The instrument recorded a dramatic drop in the intensity of the cosmic rays trapped last August, a possible sign that it had left the in the Sun’s magnetic field and a concomitant rise in that of rays generated by more Sun's sphere of influence. distant reaches of the Galaxy. That pattern indicates that Voyager 1 has travelled beyond the Sun’s magnetic influence and is no longer being shielded from galactic cosmic rays, the researchers report in a study published online this week in Geophysical Research Letters1. But if one is to believe a press release issued by NASA on 20 March (the same day the report was published), the two researchers jumped the gun. Other Voyager scientists who analysed the same data last autumn reiterate what they said then: the cosmic-ray data indicate that Voyager 1 is in a transition zone within the outer part of the heliosphere, but until a dramatic change in magnetic-field intensity and direction is detected, the craft remains firmly within the Sun’s magnetic sphere of influence. -
General Disclaimer One Or More of The
General Disclaimer One or more of the Following Statements may affect this Document This document has been reproduced from the best copy furnished by the organizational source. It is being released in the interest of making available as much information as possible. This document may contain data, which exceeds the sheet parameters. It was furnished in this condition by the organizational source and is the best copy available. This document may contain tone-on-tone or color graphs, charts and/or pictures, which have been reproduced in black and white. This document is paginated as submitted by the original source. Portions of this document are not fully legible due to the historical nature of some of the material. However, it is the best reproduction available from the original submission. Produced by the NASA Center for Aerospace Information (CASI) (NASA-CR-16S983) RESEARCH 2N PARTICLES AND V83-18777 FIELDS Semiannual Status Report, 1 Apr. - 30 Sep. 1982 (California Inst. of Tech.) 12 p HC A02/MF A01 CSCL 22A Unclas G3/12 02974 SPACE RADIATION LABORATORY CAIZORNIA INSTITUTE OF TECHNOLOGY Pasadena, California 91125 SEMI-ANNUAL STATUS REPORT for f i NA71ONAL AERONAUTICS AND SPACE ADIGNMU71ON Grant NGR 05-002-160 • "RESEARCH IN PARTICLES AND FIELDS" for 1 April 1982 - 30 September 1882 R. E. Vogt, Principal Investigator A. BuMogton, Coinvestigator 1^1 F ; ^ R L. Davis, Jr., Coinvestigator E.-C. Stone, Coinvestigator RES I ^ lurr ACM DEPT. *'NASA Technical Officer: Dr. A. G. Opp, Physics and Astronomy Programs _a_ 1 ^ TABLE OF CONTENTS Page t . Cosmic Rays and Astrophysical Plasmas 3 1.1 Activities in Support of or in Preparation for Spacecraft EnwIments 3 1.2 on NASA Spacecraft 4 2. -
The 2015 Senior Review of the Heliophysics Operating Missions
The 2015 Senior Review of the Heliophysics Operating Missions June 11, 2015 Submitted to: Steven Clarke, Director Heliophysics Division, Science Mission Directorate Jeffrey Hayes, Program Executive for Missions Operations and Data Analysis Submitted by the 2015 Heliophysics Senior Review panel: Arthur Poland (Chair), Luca Bertello, Paul Evenson, Silvano Fineschi, Maura Hagan, Charles Holmes, Randy Jokipii, Farzad Kamalabadi, KD Leka, Ian Mann, Robert McCoy, Merav Opher, Christopher Owen, Alexei Pevtsov, Markus Rapp, Phil Richards, Rodney Viereck, Nicole Vilmer. i Executive Summary The 2015 Heliophysics Senior Review panel undertook a review of 15 missions currently in operation in April 2015. The panel found that all the missions continue to produce science that is highly valuable to the scientific community and that they are an excellent investment by the public that funds them. At the top level, the panel finds: • NASA’s Heliophysics Division has an excellent fleet of spacecraft to study the Sun, heliosphere, geospace, and the interaction between the solar system and interstellar space as a connected system. The extended missions collectively contribute to all three of the overarching objectives of the Heliophysics Division. o Understand the changing flow of energy and matter throughout the Sun, Heliosphere, and Planetary Environments. o Explore the fundamental physical processes of space plasma systems. o Define the origins and societal impacts of variability in the Earth/Sun System. • All the missions reviewed here are needed in order to study this connected system. • Progress in the collection of high quality data and in the application of these data to computer models to better understand the physics has been exceptional. -
Anomalous Cosmic Rays in the Distant Heliosphere and the Reversal of the Sun’S Magnetic Polarity in Cycle 23 F
GEOPHYSICAL RESEARCH LETTERS, VOL. 34, L05105, doi:10.1029/2006GL028932, 2007 Click Here for Full Article Anomalous cosmic rays in the distant heliosphere and the reversal of the Sun’s magnetic polarity in Cycle 23 F. B. McDonald,1 E. C. Stone,3 A. C. Cummings,3 W. R. Webber,2 B. C. Heikkila,4 and N. Lal4 Received 28 November 2006; revised 5 January 2007; accepted 17 January 2007; published 7 March 2007. [1] Beginning in early June 2001 and extending over a where, by the still generally accepted paradigm, they are 3 month period the Cosmic Ray Subsystem (CRS) accelerated at the TS [Fisk et al., 1974; Pesses et al., 1981]. experiment on Voyager 1 (80.3 AU, 34°N) observed a Their relative charge composition of H, He, N, O, Ne and A rapid transition in the energy of the peak intensity of along with a small C abundance - when corrected for anomalous cosmic ray (ACR) He from 11 MeV/n to ionization rates, filtration effects and acceleration efficiency 25 MeV/n. One month later there began a similar spectral - is very similar to the abundance of neutral atoms in the shift at Voyager 2 (64.7 AU, 24°S). When these ACR local interstellar medium and their energy spectra are transition times are extrapolated back from the estimated consistent with that expected from shock acceleration at location of the heliospheric termination shock (TS) to the the TS [Cummings et al., 2002]. The heliospheric TS, which Sun (1 year) there is reasonable agreement with the range was crossed by Voyager 1 (V1) on 16 Dec. -
Cassini Mission to Saturn
NASA Facts National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, CA 91109 Cassini Mission to Saturn The Cassini mission to Saturn is the most ambi- tem. Like the other gaseous outer planets – Jupiter, tious effort in planetary space exploration ever Uranus and Neptune – it has an atmosphere made up mounted. A joint endeavor of NASA, the European mostly of hydrogen and helium. Saturn’s distinctive, Space Agency (ESA) and the Italian space agency, bright rings are made up of ice and rock particles Agenzia ranging in size Spaziale from grains of Italiana (ASI), sand to boxcars. Cassini is send- More moons of ing a sophisti- greater variety cated robotic orbit Saturn spacecraft to than any other orbit the ringed planet. So far, planet and study observations the Saturnian from Earth and system in detail by spacecraft over a four-year have found period. Onboard Saturnian satel- Cassini is a sci- lites ranging entific probe from small called Huygens asteroid-size that will be bodies to the released from aptly named the main space- Titan, which is craft to para- larger than the chute through planet Mercury. the atmosphere The 12 sci- to the surface of entific instru- Saturn’s largest and most interesting moon, Titan. ments on the Cassini orbiter will conduct in-depth Launched in 1997, Cassini will reach Saturn in studies of the planet, its moons, rings and magnetic 2004 after an interplanetary cruise spanning nearly environment. The six instruments on the Huygens seven years. Along the way, it has flown past Venus, probe, which will be dispatched from Cassini during Earth and Jupiter in “gravity assist” maneuvers to its third orbit of Saturn, will provide our first direct increase the speed of the spacecraft.