TEMPEST / EMSEC

TEMPEST controls (i.e., emissions security (EMSEC)) protect spacecraft system components, internal data communications, and communication buses against side-channel and proximity-based attacks that exploit unintended electromagnetic, electrical, or acoustic emanations. Critical components must be enclosed within appropriate casings or shielding structures that attenuate unintended emissions to levels that deny adversaries the ability to reconstruct processed data or infer system state from externally observable signals. Shielding must extend to internal buses and data pathways, not only to individual processing elements, as inter-component communications represent a significant and often overlooked emanations surface. The physical enclosure strategy must be integrated with the broader system architecture so that shielding effectiveness is not degraded by penetrations, connectors, or cable routing that create unintended emissions paths. During sustainment & maintenance, Spacecraft TEMPEST and EMSEC protections are primarily established during design, fabrication, and integration, but sustainment remains applicable through configuration control, review of deployment-state or hardware changes, preservation of qualification evidence, assessment of relevant anomalies, and evaluation of refurbishment, replacement, or follow-on production changes. The guidance below addresses these spacecraft considerations as well as applicable ground-segment maintenance activities.

Sources

ID: CM0003
Tier: II
Onboard SV CM 
Created: 2022/10/19
Last Modified: 2026/08/24

Pre-Operations Government

Acquisition requirements should establish emanations security as a design constraint applied at the system level, with specifications addressing shielding effectiveness thresholds for critical processing components, internal buses, and data communication pathways. Requirements should prohibit designs that rely solely on component-level shielding while leaving inter-component signal paths exposed. Contract language should flow TEMPEST-related design requirements to all tiers responsible for spacecraft hardware, including subcontractors supplying enclosures, harnesses, and electronic assemblies. Evaluation criteria should assess offerors' demonstrated experience with emanations-controlled design and their proposed verification methodology, including the test environments and measurement approaches to be used. Verification and validation plans should require emanations testing at representative integration stages, not only at final system acceptance, so that shielding deficiencies introduced during assembly can be identified and corrected before launch.

Pre-Operations Developer/Supplier

Emanations security must be addressed during the earliest architecture and packaging design phases, as retrofitting effective shielding after mechanical and electrical layouts are finalized is costly and often infeasible within spacecraft mass and volume constraints. Enclosure and chassis design should treat shielding effectiveness as a functional requirement alongside thermal, structural, and mass budgets, with trades documented and approved through the system design process. Printed circuit board (PCB) layout, cable routing, and connector selection should be governed by emanations control practices that minimize the emission aperture of internal signal paths. Grounding and bonding schemes must be designed to support shielding integrity rather than being treated as a purely electrical safety concern. Shielding effectiveness should be validated through measurement at the component, subsystem, and integrated spacecraft levels using test configurations that reflect the operational physical environment, including deployed configurations that may differ from ground test configurations.