SPARTA-G70

Develop geostationary orbit services using HEMERIA’s SPARTA-G70 platform, a system optimized for these orbits. 
//Scan
  • Integrated launch and propulsion interface
  • Simpler mission access
  • Deployment alone or in a constellation
  • Optimized cost and lead-time

Characteristics

Standard Model

Platform size

460 × 600 × 340 mm

Platform mass

50 kg

Max. payload mass

15-20 kg

Max. payload volume

> 70 U

Battery energy capacity

216 Wh

Payload

Mean power

Peak power

100W

200W

SADM

up to 200W

Uplink rate

10 kbps (S-band)

Downlink rate

10 kbps (S-band) · 10 Mbps (X-Band)

Delta-V

> 250 m/s

Thrust

4 x 3.2 mN

Position accuracy

10 to 20 m

Motion accuracy

1 mm/s to 2 mm/s

Attitude pointing error

0.04° à 3o

Attitude knowledge error

0.02° à 3o

Payload data storage

28 Go (Baseline) + 32 Gb (option)

Mission lifetime

> 3 years

AOCS pointing modes

Geocentric / Sun / Target / Inertial / Polynomial / From the payload.

Approved on

YODA

Two patrol smallsats

YODA

To address new threats and unfriendly actions in Space, France has a goal: to monitor Space, from Space. Against this backdrop, CNES awarded HEMERIA the YODA project (French acronym for “eyes in orbit for an agile demonstrator”), the aim of which is to design and supply a demonstrator for two reconnaissance smallsats in geostationary orbit, to protect French military satellites from suspicious, or even hostile maneuvers.

This site is registered on wpml.org as a development site.