Instrument Information |
|
IDENTIFIER | urn:nasa:pds:context:instrument:nh.sdc::1.0 |
NAME |
STUDENT DUST COUNTER |
TYPE |
DUST |
DESCRIPTION |
######################################################################## ######################################################################## REQUIRED READING: - Horanyi et al. (2007) [HORANYIETAL2007] ######################################################################## ######################################################################## The SDC description was was adapted from http://lasp.colorado.edu/sdc/ Horanyi et al. (2007) [HORANYIETAL2007], and Weaver et al. (2007) [WEAVERETAL2007] INSTRUMENT OVERVIEW =================== INTRODUCTION ------------ As the name implies, a dust counter is an instrument that counts particles of dust. There are various ways of making one work, but in the end, the instrument usally collects information on mass, velocity, density, size, or some combination of those four. The Student Dust Counter has 3 main goals. The first is to map the dust density distribution in the solar system. Dust is not spread evenly throughout space; instead, it varies in density throughout the Solar System. The first goal would be to get an accurate map of how this dust density varies. The second goal of the Student Dust Counter is to understand the dust particle size distribution and how it varies throughout the Solar System. The third main goal is to determine how fast the Kuiper Belt produces dust. The small, icy bodies in the Kuiper Belt are constantly colliding and causing little bits of each other to chip off. These little bits in turn hit each other and slowly grind into dust, in a somewhat similar fashion to how sand on a beach is created. The SDC team hopes to be able to find out how fast this is happening. SPECIFICATIONS -------------- NAME: SDC (Student Dust Counter) DESCRIPTION: Dust Counter PRINCIPAL INVESTIGATOR: Mihaly Horanyi, U. Colorado MASS RANGE: 4 picogram - 4 nanogram FIELD OF VIEW: ~ 180 deg ANGULAR RESOLUTION: N/A MASS RESOLUTION: approx factor of 2 in mass Final Name ---------- After 6 months of successful operations in space the SDC instrument was renamed, and the dedication reads: New Horizons, the first mission to Pluto and the Kuiper Belt, is proud to announce that the student instrument (SDC) aboard our spacecraft is hereby named 'The Venetia Burney Student Dust Counter' in honor of Ms. Venetia Burney Phair, who at age of eleven nominated the name Pluto for our solar system's ninth planet. May 'Venetia' inspire a new generation of students to explore our solar system, to make discoveries which challenge the imagination, and to pursue learning all through their lives. In this archive, the name Student Dust Counter and the acronym SDC will continue to be used. Scientific Objectives ===================== The Student Dust Counter (SDC) will count and measure the sizes of dust particles along New Horizons' entire trajectory, which covers regions of interplanetary space never before sampled. Such dust particles are created by comets shedding material and Kuiper Belt Objects colliding with one another. The SDC is managed and was built primarily by students at the University of Colorado in Boulder, with supervision from professional space scientists. Calibration =========== See Horanyi et al. (2007) [HORANYIETAL2007], especially sections 3.4.3 and 3.5. Operational Considerations ========================== SDC was designed to take advantage of the quiet state of the spacecraft during cruise phase. Various active spacecraft operations cause mechanical shocks that are picked up by the polyvinylidene fluoride (PVDF) sensors and registered by SDC as science events. This is particularly true during three-axis pointing and active spin mode when the spacecraft frequently fires short bursts of the attitude thrusters. Level four data reduction (section 4 of Horanyi et al. (2007) [HORANYIETAL2007]) is used to filter out any hits that appear within a second of any thruster firing, thereby allowing science recovery between firings. However because the thruster induced events are often frequent enough to violate the autonomy rule B (section 3.4.2 of Horanyi et al. (2007) [HORANYIETAL2007]), during spacecraft manuvers many SDC detector channels switch off for prolonged periods. During the first six months of flight, there are several periods, some weeks or months long, where SDC was completely off. Detector ======== The SDC's sensors are thin, permanently polarized PVDF plastic films that generate an electrical signal when dust particles penetrate their surface. The SDC has a total sensitive surface area of ~0.1 m^2, comprising 12 separate film patches, each 14.2 cm x 6.5 cm, mounted onto the top surface of a support panel. In addition, there are two reference sensor patches mounted on the backside of the detector support panel, protected from any dust impacts. These reference sensors, identical to the top surface sensors, are used to monitor the various background noise levels, from mechanical vibrations or cosmic ray hits. Electronics & Construction ========================== The Student Dust Counter comprises three major pieces: The Detector Assembly is 18 inches x 12 inches (46cm x 30cm). This is the piece of equipment that is mounted on the outside of the spacecraft and is exposed to the dust particles. The detector is thermally isolated from the New Horizons Spacecraft and lies outside its Thermal Blanket. The Electronics Box is approximately 5.4 inches x 8.25 inches x 1.825 inches (13.7cm x 20.96cm x 4.64cm). This is the brains of the Dust Counter; when a hit occurs on the detector the electronics box will decipher the data and determine the mass and speed of the dust particle. The electronics box is actually located within the spacecraft and is thermally and electronically bonded to the New Horizons Spacecraft. The Intra-Harness is the 'bridge' between the detector assembly and the electronics box. It serves a similar purpose as the cable which allows your home computer to communicate with your printer. The space environment through which the New Horizons Mission will be traveling contains a large variety of conditions which can negatively affect spacecraft materials. The dust collector must be made of a substance which is not affected by changes in the temperature, radiation environment, or quantity of high-energy particles surrounding it. To meet these challenges, a simple, reliable substance called PolyVinyliDene Fluoride (PVDF) has been chosen. When PVDF is manufactured, it is polarized. This means all of the molecules in the material are aligned so that they are pointing in the same direction. When a dust particle impacts on the detector, it randomly aligns some of these previously organized molecules. This depolarization generates an electric signal which is then detected. The pulse height of the signal indicates the mass of the dust particle using the relative velocity of the spacecraft. Operating Modes =============== Data taking and Calibration. See Horanyi et al. (2007) [HORANYIETAL2007] for details. Measured Parameters =================== The SDC measures and/or records four parameters for each Interplanetary Dust Particle (IDP) impact event: charge (generated by each event); time; count; sensor (channel) number. Masses and velocities of IDPs may be inferred from the measured charge of events detected by the SDC sensors. |
MODEL IDENTIFIER | |
NAIF INSTRUMENT IDENTIFIER |
not applicable |
SERIAL NUMBER |
not applicable |
REFERENCES |
Superseded by [HORANYIETAL2008], Horanyi, M., V. Hoxie, D. James, A. Poppe, C.
Bryant, B. Grogan, B. Lamprecht, J. Mack, F. Bagenal, S. Batiste, N. Bunch, T.
Chantanowich, F. Christensen, M. Colgan, T. Dunn, G. Drake, A. Fernandez, T.
Finley, G. Holland, A. Jenkins, C. Krauss, E. Krauss, O. Krauss, M. Lankton, C.
Mitchell, M. Neeland, T. Resse, K. Rash, G. Tate, C. Vaudrin, and J. Westfall,
The Student Dust Counter on the New Horizons Mission, Space Sci. Rev., Volume
140, Numbers 1-4, pp. 387-402, 2008. Superseded by [WEAVERETAL2008], Weaver, H.A., W.C. Gibson, M.B. Tapley, L.A. Young, and S.A. Stern, Overview of the New Horizons Science Payload, Space Sci. Rev., Volume 140, Numbers 1-4, pp. 75-91, 2008. |