a.i. solutions engineers and subject matter experts have supported a variety of launch vehicles (e.g. Atlas II/V, Delta II/IV, Pegasus XL, Taurus XL/2, Falcon 1/9, Minotaur I/IV), performing launch vehicle trajectory design and optimization, GN&C control algorithm design and verification, structural and thermal environment assessments, ground and flight software independent validation and verification (IV&V), and other mission analyses as well as on-console support.
We also support launch vehicle certification, performing independent technical assessments of launch vehicle designs, hardware qualification, and mission assurance reviews to ensure flight worthiness of the hardware components and the end system.
We provide mission assurance expertise in the areas of trajectory modeling; GN&C; thermal evaluations of liquid and solid propulsion systems; structural loading, fatigue, and dynamic environments evaluations; and electromagnetic interference/ compatibility (EMI/EMC) for avionics, sensors, and other electronic components and systems. We provide expertise in environmental requirements specifications and testing.
In support of spacecraft and missile sensor design, a.i. solutions participates in the development of major systems. We perform analyses, simulating missiles with both liquid and solid rocket motor systems, to verify missile performance and to demonstrate that mission requirements will be met. We also perform independent loads analyses to verify that structural margins are adequate for all critical areas on the missile.