SAC has put out an EOI asking Indian industry to take over full assembly, integration and testing (AIT) of its electro-optical imaging payloads. That's the whole job, from receiving bare mirrors to handing over a calibrated, TVAC-tested camera at URSC.
EOI no. SAC/EOI/03/D/2026-27, issued 30 Oct, responses due 30 Nov 2026 by 3 PM IST.
It covers 14 payloads across 5 types. SAC doesn't name the missions, but the optics specs give away quite a lot:
> Type-2, "Cartographic Imager" (4 units)
1.2 m Korsch telescope, ~16 m focal length, PAN/MX/MWIR/SWIR
→ Same 1.2 m optics class as Cartosat-3. A 16 m focal length works out neatly for its 0.25 m GSD from 509 km.
> Type-3, High Resolution Imager (3 units)
Two-mirror Ritchey-Chrétien, 600 mm primary, ~5.8 m focal length, PAN/MX + MWIR, LWIR and night-time light imaging, with an onboard blackbody for calibration
→ Basically the Cartosat-2 telescope layout (700 mm, 5.6 m). Closest published spec we could find is HRSAT (1 m PAN, 4 m MX, 20 m LWIR).
> Type-1, Wide Swath High Resolution Imager (3 units)
~1.13 m mirror but only ~3.5 m focal length, nine butted detectors plus four MWIR chains, ~700 kg optics module (roughly what an entire Cartosat-2 satellite weighed)
→ Big, fast optics built for swath and signal, not Cartosat-style narrow-strip imaging. We couldn't match it to any announced ISRO mission.
> Type-4, "Advanced Resource Monitoring Satellite" (2 units)
Two TMA telescopes, fore and aft, ~2 m focal length, fixed pitch bias
→ The Cartosat-1 stereo layout (two TMAs, 1.945 m, +26/-5 deg), which Resourcesat-3S/3SA carries forward.
> Type-5, "Advanced Resource Monitoring Satellite" (2 units)
VNIR+SWIR side modules, a central TMA module and three hyperspectral heads
→ Lines up with Resourcesat-3/3A: ALISS-3 at 20 m on the sides and 10 m in the centre, plus ATCOR.
The vendor's scope covers stress-free bonding of mirrors onto CFRP structures, interferometric telescope alignment, detector focusing, integrating the electronics, harness and thermal hardware, TVAC and vibration testing, and full calibration (MTF, SNR/NEDT, band-to-band registration, spectral, radiometric). Then delivery to URSC Bengaluru and support right through in-orbit testing.
How it works:
> Phase-1: training at SAC + building all the ground support equipment
> Phase-2: first unit of each type built at SAC, vendor team under SAC supervision
> Phase-3: remaining units at the vendor's own facility
→ At least ~16 months per payload, contract runs about five years.
The entry bar is high:
> Own ISRO-approved ISO 8 cleanroom, 30 m x 20 m per payload type, with an ISO 7 optical bay
> TVAC chamber with an optical window (shroud -100 to +70 C, 10^-6 torr)
> 1.5 m class collimator, reference flat, integrating sphere and blackbody
> Prior AIT experience on an EO imager above 200 mm aperture
> At least five years as a company, no consortiums
> If flight hardware gets damaged during AIT or transport, the vendor pays
This comes after SAC's 2025 EOIs for focal plane assemblies and MWIR detector-cooler assemblies. Bit by bit, the EO payload chain is moving to industry, while SAC keeps design authority and final acceptance.
(Mission matches are our reading of the optics specs and published mission data. The EOI itself doesn't name any.)
Archived:
indianspaceflight.in/archive…
Source:
isro.gov.in/media_isro/pdf/T…
#ISRO #Cartosat #Resourcesat #EarthObservation