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The Dipper Satellite: A Medium-Class Explorer Mission to the Threshold of SpaceThe Dipper satellite will carry out an unprecedented, systematic, and focused in-situ exploration of the Earth's lower ionosphere and thermosphere below 200 km that will produce a pivotal base of knowledge that will significantly advance our understanding of knowledge that will significantly advance our understanding of how our near-space environment works. The satellite will carry comprehensive in-situ probes to measure vector electric and magnetic fields, plasma density and temperature, ion velocities, ion and neutral composition and winds, energetic particles including suprathermal electrons, gravity waves, and lightning bursts. The satellite will include a propulsion system and tapered body that will provide over 10,000 excursions to altitudes below 200 km with over 3000 dips to altitudes below 150 km. With this instrument complement, spacecraft, and orbit, the Dipper mission will gather the necessary combined electrodynamics and neutral dynamics measurements to provide an understanding of the Earth's critical boundary region where the ionized gases of space and the neutral gases of the atmosphere are coupled, and where impinging forces and momentum are deposited from the magnetosphere above and from the troposphere, stratosphere, and mesosphere below. In exploring those physical processes in the lower ionosphere which can only be measured in-situ, the Dipper mission addresses four main science objectives. The Dipper will: 1) reveal how ion-neutral coupling creates a global system of dynamo electric fields and currents; 2) provide first-hand understanding of how magnetospheric currents close in the ionosphere and reveal the effects on the upper atmosphere of magnetospheric energy and momentum deposition; 3) discover the degree of upwards coupling and energy deposition due to thunderstorm electric fields and determine their significance; 4) determine the dynamics and composition of the Earth's lower thermosphere, including its response to gravity, tidal, and planetary waves on a range of spatial scales. A proposal to design, build, operate, and analyze data from instruments on the Dipper spacecraft within the schedule and budget constraints of NASA's MIDEX program was submitted to NASA in 1998. This presentation summarizes the main features of the mission.
Document ID
20000012312
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Pfaff, R. F., Jr.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Acuna, M.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Bounds, S.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Hoffman, R.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Mahaffy, P.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Earle, G.
(Texas Univ. Dallas, TX United States)
Fesen, C.
(Texas Univ. Dallas, TX United States)
Heelis, R.
(Texas Univ. Dallas, TX United States)
Blake, J.
(Aerospace Corp. El Segundo, CA United States)
Christensen, A.
(Aerospace Corp. El Segundo, CA United States)
Clemmons, J.
(Aerospace Corp. El Segundo, CA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1999
Subject Category
Geophysics
Meeting Information
Meeting: American Geophysical Union Fall Meeting
Location: San Francisco, CA
Country: United States
Start Date: January 1, 1999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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