5th Annual CubeSat Developers' Workshop April 2008 Cal Poly San Luis Obispo, California
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1 5th Annual CubeSat Developers' Workshop 9-11 April 2008 Cal Poly San Luis Obispo, California From UNISAT to ubesatsat UNICube Chantal CAPPELLETTI, Fabrizio PAOLILLO, Francesco GUARDUCCI, Luigi RIDOLFI Filippo GRAZIANI, Paolo TEOFILATTO, Fabio SANTONI, Fabrizio PIERGENTILI, Maria Libera BATTAGLIERE Scuola di Ingegneria Aerospaziale SAPIENZA, Università di Roma Gruppo di Astrodinamica dell Università degli Studi la Sapienza
2 Satellite S. Marco 1 (Scout, Wallops Island) December 15, 1964 S. Marco Equatorial Range
3 Launches from San Marco Equatorial range Date Satellite Payload April 26, 1967 San Marco 2 December 12, 1970 Small Astronomy Satellite (SAS) 1, Uhuru April 24, 1971 San Marco 3 November 15, 1971 Small Scientific Satellite (SSS) 1 November SAS 2 February 18, 1974 San Marco 4 October 15, 1974 UK-5 May 8, 1975 SAS 3 March 25, 1988 San Marco 5 Thermosphere analysis X rays sources Thermosphere analysis Van Allen belts electrical and magnetic fields Gamma rays sources Thermosphere analysis X rays sources Thermosphere analysis
4 A short history of UNISAT program Theoretical studies on building low-cost microsatellites at university A few people trusted it was possible that students could design realize microsatellites using commercial off-the the-shelf components 1995 First grant to UNISAT program received from Italian Ministry of University Building of ground station (SPIV) researchers of University of Rome at Stanford University 1997 Design and realization of UNISAT start 2000 Launch of UNISAT
5 UNISAT microsatellites Unisat 26 Sept Unisat-2 20 Dec Unisat-3 29 Jun Unisat-4 26 Jul. 2006
6 Design and realization of electronic boards Solar arrays manufacturing Structure design and manufacturing Ground tests, integration, launch and operation in orbit
7 Test campaign
8 Integration at the Baikonour Cosmodrome
9 Launch UNISAT 3
10
11 Launch site
12 Launch groups
13 Publications Papers Thesis Quaderni di Astrodinamica GAUSS Activities Space Education through hands-on experience since 1990 Astrodynamics laboratory Mission Analysis SPIV Ground Station Microsatellites UNISAT Space debris Guidance, Navigation and Control
14 Today Activities Unisat-5 UNICubeSAT Edusat
15 Epsilon (Narcissus) Students payload NARCISSUS - the satellite that pictures itself Take pictures of UNISAT from a camera located on the TIP MASS of a gravity gradient boom (EPSILON) EPSILON structure has been already designed, built and tested 1W average power 1 kg weight 10x10x10cm 1 liter volume PIC micro Wireless connection to UNISAT EPSILON NARCISSUS
16 ubesat Experiments UNICube The VEGA MAIDEN flight Cubesat orbit (350x1200km) has unique characteristics for: Atmospheric density measurement (low altitude perigee) Radiation environment measurements (High altitude apogee)
17 Atmospheric density evaluation from UNISAT, UNISAT-2 2 and UNISAT-3 global semiaxis data Semiaxes [km] UNISAT, UNISAT 2 and UNISAT 3 semiaxis variation a a 2 3 ρv SC = mµ D Atmospheric density [Kg/m3] x Density variations evaluated by UNISAT, UNISAT 2 and UNISAT 3 semiaxis decreasing UNISAT 3 UNISAT 3 peaks UNISAT 2 UNISAT 2 peaks UNISAT UNISAT peaks Days from launch of UNISAT U.S. Dept. of Commerce, NOAA, Space Environment Center [Joules/second/square meter/hertz] Days from launch of UNISAT Flusso solare a 10.7 cm Solar flux 10.7 cm Data
18 Thermosphere analysis (atmospheric density) from local measurements and orbital velocity data The Broglio Theory Broglio Drag Balance (dynamometer concept) m1 Traditional accelerometer concept
19 UniCubesat implementation of the Broglio Drag Balance concept
20 Displacement sensor (preliminary selection)
21 Space Debris Project
22 SIRDARIA Spacecraft Integrated Re-entry Device Aero-Resistant, Increasing Area
23 Infrastructures: Dome lightness (max 8 kg) easy to transport fast to assemble (2 hours) modularity completely automated remotely controlled
24 OPTICS/1 CASSEGRAIN MODIFIED, 400 mm, f/1.8.
25 OPTICS/2 BAKER-SCHMIDT 300 mm, f/2.8
26 Space debris optical observation and orbital determination USCT Unsuccesfully Correlated Object Rocket Body Cat. n Pleiadi + LEO Uncontrolled Satellite Marecs 2B GEO Satellites Hot Bird 1 to 5 GEO Satellites HOT BIRD 1-5
27
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