Propeller and Engine Load Analysis

The contract titled Propeller and Engine Load Analysis requires the detailed conduct and delivery of load and thrust analysis for an engine system, with specific focus on predicted engine load and thrust output under operational conditions. The analysis must be benchmarked against the original equipment manufacturer's performance limits of 588 kW or 800 horsepower at 2100 rpm, ensuring compliance with established technical thresholds. All findings must be thoroughly documented and presented in a manner that supports technical decision-making and system validation. This subcontract is issued by the Government of Canada through the Royal Canadian Mounted Police, with performance expected to take place in British Columbia. The solicitation was posted on June 18, 2026, and responses must be submitted by July 21, 2026. The contract falls under NAICS code 541690, indicating it involves other scientific and technical consulting services. The work is part of a broader procurement initiative by the Canadian government, targeting specialized engineering analysis to support aviation or marine propulsion system integrity. All deliverables must meet the required technical standards without reliance on external documentation references.