MSS Omnispyre: Difference between revisions

**MSS Omnispyre**
	MSS Aphrodite
Function	Optical Imaging/SIGINT Satellite
Place of origin	Nouvelle Alexandrie
Designed	Minerva Space Systems
Manufacturer	Minerva Space Systems
Dimensions	11.0 m x 10.5 m x 4.1 m
Launch Mass	19,600 kg
Electrical Power	5.7 kW
Telemetry	V Band
Attitude control	Three-axis momentum biased
Propulsion	16x N2O4/MMH RCS thrusters, 18 N each; 2x N2O4/MMH main engines, 1000 N each;
Instruments	Three-mirror anastigmat telescope (3.2 m mirror, 0.08 m resolution); Wide-Field-of-View Camera (WIDECAM); 18 x Visible/NIR Si CCD, 4096 x 4096 px, 0.2 to 1.1 μm; High-Resolution Camera (HIGHCAM); 2 x Visible/NIR Si CCD, 2048 x 4096 px, 0.2 to 1.1 μm; 1 x MWIR/LWIR HgZnTe FPA, 1040 x 1040 px, 3 to 5 and 8 to 12 μm; 2 x Omnidirectional SIGINT Antennae (0.01 to 110 GHz);
Orbital parameters	Orbit height: 820 km; Orbit inclination: 97 degrees; Orbit life: 10-12 years;

Revision as of 16:38, 13 March 2023

The MSS SpecSat is an advanced electro-optical and SIGINT reconnaissance satellite designed by Javelin Industries's space subsidiary, Minerva Space Systems.

Revision as of 16:37, 13 March 2023 view source Edgard (talk \| contribs) 35,068 edits Created page with "{{Nouvelle Alexandrie Article}} {{ infobox \| bodyclass = toccolours \| bodystyle = float:right; margin: 0 0 1em 1em; font-size: 85%; width: 30em;background-color:#C0C0C0;..."	Revision as of 16:38, 13 March 2023 view source Edgard (talk \| contribs) 35,068 edits m Edgard moved page MSS SpecSat to MSS Omnispyre Newer edit →
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