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| <HTML> | |
| <HEAD> | |
| <META NAME="GENERATOR" CONTENT="Adobe PageMill 3.0 Win"> | |
| <TITLE>International Program Office -SXG Project</TITLE> | |
| </HEAD> | |
| <BODY TEXT="#000099" BGCOLOR="#ffffff" VLINK="#990099"> | |
| <P><CENTER><TABLE WIDTH="577" BORDER="0" CELLSPACING="2" CELLPADDING="0"> | |
| <TR> | |
| <TD WIDTH="36%"> | |
| <IMG SRC="../../../images/sxg_lg.gif" WIDTH="188" HEIGHT="135" | |
| ALIGN="BOTTOM" BORDER="0" NATURALSIZEFLAG="0"></TD> | |
| <TD WIDTH="64%"> | |
| <P><CENTER><B><FONT COLOR="#ff0000" SIZE="+2" FACE="Arial"><IMG | |
| SRC="../../../images/INTL_SXG_Title_LG.jpg" WIDTH="360" HEIGHT="126" | |
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| </TR> | |
| <TR> | |
| <TD COLSPAN="2"> | |
| <P> </P> | |
| <P><FONT SIZE="-1" FACE="Arial">The SXG is an international collaborative | |
| mission between Russia, various international partners in Europe | |
| and NASA. The spacecraft and launch vehicle will be provided | |
| by IKI of Russia. The mission will carry two U.S. nstruments: | |
| a Stellari X-Ray Polarimeter (SXRP) focal plane instrument and | |
| a wide field Monitoring X-Ray Experiment (MOXE).</FONT></P> | |
| <P><FONT SIZE="-1" FACE="Arial">SXRP objective is to perform | |
| x-ray polarization measurements addressing a number of astrophysical | |
| problems including X-ray pulsars, black holes, accretion disk | |
| scattering, radio pulsars, supernova remnants and active GALACTIC | |
| NUCLEI. The SXRP energy band is from 2.6 KeV to 12 KeV.</FONT></P> | |
| <P><FONT SIZE="-1" FACE="Arial">MOXE objective is two fold: First, | |
| to alert observers on Spectrum-X-Gamma and other platforms of | |
| interesting<BR> | |
| transient x-ray events. Second, to synoptically monitor the X-ray | |
| sky and study long-term changes in X-ray binaries and other compact | |
| objects. MOXE will be sensitive to sources as faint as 2 millicrab | |
| and will cover the wavelength range from 2-12 KeV.</FONT></P> | |
| <P><B><FONT SIZE="-1" FACE="Arial">Salient Features:</FONT></B></P> | |
| <P><B><FONT SIZE="-1" FACE="Arial">Project Start: </FONT></B><FONT | |
| SIZE="-1" FACE="Arial">1989 <B><BR> | |
| Spacecraft Weight: </B>5700 kg <B><BR> | |
| Planned Lifetime: </B>3 years<B> <BR> | |
| Orbit: </B>500 Km X 200,000 Km, 51.50 inclination<B> <BR> | |
| Launch: </B>Proton from Baikanur, Russia, TBD</FONT></P> | |
| <P><B><FONT SIZE="-1" FACE="Arial">Instrument Complement:</FONT></B></P> | |
| <P><FONT SIZE="-1" FACE="Arial">Jet-X (UNITED KINGDOM) <BR> | |
| Euvita (SWITZERLAND) <BR> | |
| Six-A (FINLAND) <BR> | |
| MOXE (NASA/LANL) <BR> | |
| HEPC/LEPC <BR> | |
| TAUVEX (ISRAEL) <BR> | |
| SXRP (NASA/CU) <BR> | |
| MART (ITALY) <BR> | |
| KFRD (RUSSIA) <BR> | |
| RIUS (HUNGARY) <BR> | |
| DSI (DENMARK)</font> | |
| </TD> | |
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