OPAG Update to the Planetary Science Advisory Committee (PAC)
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Revolutionizing Solar System Science with WFIRST
! Revolutionizing Solar System Science with WFIRST Bryan J. Holler WFIRST Solar System Working Group (SSWG) Stefanie Milam Ernesto Palomba James Bauer Silvia Protopapa Charles Alcock Lynnae Quick Michele Bannister Darin Ragozzine Gordon Bjoraker Vishnu Reddy Dennis Bodewits Jason Rhodes Amanda Bosh Andy Rivkin Marc Buie Gal Sarid Tony Farnham Amanda Sickafoose Nader Haghighipour Amy Simon Paul Harderson Cristina Thomas Alan Harris David Trilling Henry Hsieh Robert West Michael Kelley With thanks to: Matthew Knight Christopher Hirata Emily Kramer Jason Kalirai Andrea Longobardo Jeff Kruk Conor Nixon Ed Nelan “Observations of XYZ will provide valuable information for understanding the origin and evolution of the solar system.” -Every solar system proposal Not to scale! Discovery Characterization WFIRST mission assumptions No IFC No moving target tracking Passive cooling Surveys not yet finalized Descope effects on solar system science Holler et al. (2018) NASA/JPL/K. McGill Estimated detection limits (1000 sec, 5-σ) Holler et al. (2018) Mining the astrophysics surveys Microlensing survey 8 Size-Frequency Distribution 44,555 Main Belt Asteroids 6 4 Log Frequency 2 0 0 5 10 15 20 25 30 Diameter (km) 120 ~1500 asteroids per W149 AB mag 100 square degree 80 ≈ 60 Johnson V Vega 40 Frequency per square degree 20 mag 0 15 20 25 30 35 W149(AB) magnitude Microlensing survey (cont.) • Gould (2014) claims: • Detection of KBOs down to V=30.2 • Detection of KBO satellites w/n 10 mas of primary down to V=31.0 • Cadence of microlensing survey could result in the construction of rotation light curves High-Latitude Survey (HLS) • DES and LSST can reach r<24.5 • WFIRST will be able to reach r<27 • Observe targets 3x smaller at a particular distance or 3x farther away for a particular size Spergel et al. -
NASA's Dragonfly Program: Commercialized Robotics
35th Space Symposium, Technical Track, Colorado Springs, Colorado, United States of America Presented on April 8th, 2019 NASA’s Dragonfly Program: Commercialized Robotics - Enabling a New Generation of Evolvable, Resilient Assets in Orbit John Lymer Maxar† Abstract Commercialized, affordable robotics for in-space assembly of large platforms and structures are being prepared for flight in 2021. Integrating easily with standard GEO and LEO satellite command and control architectures, these automation systems enable a new operating paradigm for on-orbit assets – one that includes incremental growth, on-demand payload refresh to match user needs, and in-situ warehousing for rapid expansion, augmentation, or dispersion on a timeline independent of launch. Introduction The Dragonfly Robotic System, developed first as a DARPA seedling and then maturing through the NASA Tipping Point Program, successfully completed a ground demonstration in late 2017, shown in Figure 1 assembling a Ka band antenna. Critical Design Review occurred in 2018. Ultra-lightweight and affordable, the Dragonfly Robotic System is designed to fit into existing satellite command and data handling (C&DH) subsystems and low rate command/telemetry links for inexpensive integration – it behaves like any other satellite subsystem. The supervised autonomy operating concept facilitates command and control from a standard Mission Operations Center. Current satellite operations personnel can plan and execute robotic operations with only minor additional training. Dragonfly represents the first ‘commercialized’ robotic system – affordable and accessible to satellite owners without the risk of infrastructure changes. † The operations of DigitalGlobe, SSL and Radiant Solutions were unified under the Maxar brand in February. MDA continues to operate as an independent business unit within the Maxar organization. -
An Impacting Descent Probe for Europa and the Other Galilean Moons of Jupiter
An Impacting Descent Probe for Europa and the other Galilean Moons of Jupiter P. Wurz1,*, D. Lasi1, N. Thomas1, D. Piazza1, A. Galli1, M. Jutzi1, S. Barabash2, M. Wieser2, W. Magnes3, H. Lammer3, U. Auster4, L.I. Gurvits5,6, and W. Hajdas7 1) Physikalisches Institut, University of Bern, Bern, Switzerland, 2) Swedish Institute of Space Physics, Kiruna, Sweden, 3) Space Research Institute, Austrian Academy of Sciences, Graz, Austria, 4) Institut f. Geophysik u. Extraterrestrische Physik, Technische Universität, Braunschweig, Germany, 5) Joint Institute for VLBI ERIC, Dwingelo, The Netherlands, 6) Department of Astrodynamics and Space Missions, Delft University of Technology, The Netherlands 7) Paul Scherrer Institute, Villigen, Switzerland. *) Corresponding author, [email protected], Tel.: +41 31 631 44 26, FAX: +41 31 631 44 05 1 Abstract We present a study of an impacting descent probe that increases the science return of spacecraft orbiting or passing an atmosphere-less planetary bodies of the solar system, such as the Galilean moons of Jupiter. The descent probe is a carry-on small spacecraft (< 100 kg), to be deployed by the mother spacecraft, that brings itself onto a collisional trajectory with the targeted planetary body in a simple manner. A possible science payload includes instruments for surface imaging, characterisation of the neutral exosphere, and magnetic field and plasma measurement near the target body down to very low-altitudes (~1 km), during the probe’s fast (~km/s) descent to the surface until impact. The science goals and the concept of operation are discussed with particular reference to Europa, including options for flying through water plumes and after-impact retrieval of very-low altitude science data. -
Overview of Dragonfly Entry Aerosciences Measurements (Dream) J
Overview of Dragonfly Entry Aerosciences Measurements (DrEAM) J. Santos1, A. Brandis2, H. Hwang1, A. Gülhan3, T. Thiele3, F. Siebe3, 1NASA Ames Research Center, Moffett Field, CA 94035, USA; 2AMA, Inc. at NASA Ames Research Center, Moffett Field, CA 94035, USA; 3German Aerospace Center (DLR e.V.), Supersonic and Hypersonic Technologies Department, Linder Höhe, 51147 Köln, Germany. Abstract: NASA Ames Research Center (ARC) (COSSTA). Since the methane concentration in the Ti- leads the Dragonfly Entry Aerosciences Measurements tan atmosphere is directly proportional to the radiative (DrEAM) project, which is an aeroshell instrumentation heat flux, the COSSTA measurements will be used to suite on the Dragonfly mission that fulfills the Engineer- reduce the current uncertainty in the methane volume ing Science Investigation requirement for the New fraction. Atmospheric density measurements and cap- Frontiers mission. NASA ARC is partnering with sule aerodynamic data will be obtained through the NASA Langley Research Center (LaRC) and the Ger- onboard Inertial Measurement Unit (IMU), supple- man Aerospace Center (DLR) to provide a comprehen- mented by pressure transducers similar to those used by sive sensor suite, including a DLR-provided Data Ac- the MEDLI and MEDLI2 projects. The DrEAM pres- quisition System (DAS). DrEAM will provide key aer- sure sensors will be known as the Dragonfly Atmos- othermodynamic data and performance analysis for pheric Flight Transducers. (DrAFT). The pressure Dragonfly’s forebody and backshell Thermal Protection measurements, when combined with data from the on- System (TPS). board IMU, will allow for reconstruction of such quan- Titan’s atmosphere predominantly consists of nitro- tities as vehicle Mach number, freestream density, and gen (~98% by mole) with small amounts of methane atmospheric winds. -