Argentine National Space Plan - ITU · PDF fileS.C.de Bariloche, Argentina 29 to 31 May 2017...

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ITU International Satellite Symposium 2017 S.C.de Bariloche, Argentina 29 to 31 May 2017 [email protected] Argentine National Space Plan

Transcript of Argentine National Space Plan - ITU · PDF fileS.C.de Bariloche, Argentina 29 to 31 May 2017...

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ITU International Satellite Symposium 2017

S.C.de Bariloche, Argentina 29 to 31 May 2017

[email protected]

Argentine National Space Plan

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• “To go to space to know Earth better”

• “An opportunity for the national technology

development”

The Argentine Space Program

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Information cycles for:

agriculture, fishing and forest activities

climate, hydrology and oceanography

monitoring of the environment and natural resources

cartography, geology and mining production

disaster management

health applications

national security

The National Space Program

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CETT: Centro Espacial Teófilo Tabanera

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Environmental

Test Facilities

CETT (Laboratorios)

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CONAE in Space

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Argentine Payloads

Institutions:

CONAE

UNLP

IAR

CIOP

GEMA

Companies:

INVAP

VENG

STI

DTA

CRUX

DCS

TDP

MWR HSCNIRST

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Solar Panels (CNEA)

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Integration Room (INVAP)

INVAP, Bariloche, June 14, 2010.

SAC-D/Aquarius Integration

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SAOCOM Mission Objectives

soil moisture maps (hydrology-

including floods, agriculture, climate

and health)

information extraction using SAR

interferometry capability (terrain

modeling, terrain displacement

mapping, volcanology, etc.)

emergencies and other applications

from the Information Cycles of the

National Space Program

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MASS BUDGET:

2800 kg wet mass at launch (+200kg system margin)

DIMENSIONS:

h = 4.468m 2.965m stowed envelope

10m x 3.5m (35m2) SAR Active Phase Array antenna

15m2 foldable solar array wing

CONFIGURATION:

Two Satellites with L-Band SAR Instrument

as main instrument

Orbit : 619.6 km

Near Polar Sun-synchronous frozen orbit,

06:00 am ascending node

SAOCOM

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Project Status

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Project Status

Solar Simulator Test Campaign Finalized

IABG(Germany)

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SAR Antenna Panels at LIE (CONAE – CETT)

Mayo 2016

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Platform Integration of SAOCOM 1A

INVAP S.E. Bariloche

SAOCOM 1A launch March 2018

SAOCOM 1B launch 1 year later

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Constelation of 6 satellites with SAR instruments

on board, 4 italian in X band (COSMO-SkyMed)

and 2 argentinean in L band (SAOCOM):

Multiband synergy (X & L)

High revisit (12 hs)

SIASGE

Benefits:

Excellent synergy between and L band data, which

represents a key for satisfying the different user needs

Significant improvement in the accuracy of the

discrimination among the different surface components

Significant improvement in the geophysical parameters

quantitative knowledge

Very high revisit for monitoring events of fast evolution

Improvement in cartographic and change detection studies

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Main Payloads:

• Super-spectral Camera, with 19 bands in the Visible, SWIR, and Thermal ranges, with

200m pixel resolution, and daily repetition rate, for coastal studies and south American

continental territory.

• Similar, but with 1 km pixel resolution, daily repetition rate and global coverage.

Next Steps (1): SABIA-Mar

Objective:

To study the Oceanic Biosphere,

its changes along time, and how

it is affected and reacts to human

activities.

SABIA-Mar 1 and 2

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Next Steps (2): Segmented Architecture

1. Small satellites in a network

2. Cluster concept

3. Sharing of Resources

4. Distributed Processing

5. Distributed Payloads

6. Advanced Communications

Flexible to requirement changes

Flexible to changes in technology

Shortens the Mission cycle times

Lower Mission costs

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High Resolution Mission (1 meter panchromatic, 5 meters multispectral)

4 Satellites in polar sun synchronous orbit

Revisit time better than 8 days

Next Steps (3): SARE AR-1

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TII Requirements

• Polar Orbit

• Altitude 600 km

• Weights up to 250 kg

• Under Development in Argentina

• Launch site in Argentina

TII Requirements

• Polar Orbit

• Altitude 600 km

• Weights up to 250 kg

• Under Development in Argentina

• Launch site in Argentina

Length and weight:

Empty :

Diameter :

Thrust 1st stage :

Thrust last stage :

28 m and 67 ton

5,1 ton

2,5m

90ton

4ton

Main Characteristics:

Next Steps (4): Launch Vehicle TII

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Next Steps (6): Launch Base

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Thanks