Vertex Aerospace, LLC

Aerospace Thermal Engineering

Website

About the firm

Vertex Aerospace, LLC is a Maryland-based thermal engineering practice co-founded in 2010 by University of Maryland alumni with more than 60 years of combined experience supporting NASA, DoD, and commercial space programs. Specializing in the full-cycle thermal control system (TCS) workflow - design, analysis, integration, and test - it serves customers including NASA Goddard Space Flight Center, NOAA, Johns Hopkins University Applied Physics Laboratory, and Southwest Research Institute. A structured mentoring model and sustained investment in the next generation of engineers underpin its approach to high-quality, cost-effective aerospace thermal engineering.

Established
2010
Team
Small
Firm type
Aerospace Engineering · Thermal & Heat Transfer

People

Nicholas M. TetiPresident/CEO

Rommel N. ZaraVice President/CTO

Evan T. AlexanderSr. Thermal Engineer

Mark C. AukermanThermal Engineer

Ethan T. BurbridgeThermal Engineer

Michael D. CommonsSr. Thermal Engineer

Thomas (Richard) DodgeSr. Thermal Engineer

Jong S. KimChief Thermal Engineer

Kevin B. KimChief Thermal Engineer

Shannon G. MacmasterThermal Engineer

Emily A. MaherasThermal Engineer

Carson S. McDonaldSr. Thermal Engineer

Gilbert (Wes) OusleyChief Thermal Engineer

Matthew R. PatsyThermal Engineer

John K. RitzJr. Thermal Engineer

Santino V. RosanovaSr. Thermal Engineer

Jason A. SolimaniThermal Subject Matter Expert

Nico TetiAdministrative Manager

Jordan L. ThompsonSr. Thermal Engineer

Travis FrazierSenior Thermal Engineer

Capabilities

Thermal Control System Design

Service website

End-to-end TCS design for spacecraft, instruments, and components - from thermal requirements definition and hardware specifications to interface control documents and satellite integration leadership.

  • Requirements Definition and Management

    Defining, documenting, and managing lower-level thermal requirements; negotiating subsystem interfaces; and maintaining subsystem cost and schedule baselines.

  • TCS Hardware Specifications

    Writing hardware specifications and procurement details; developing design concepts and thermal control options for components, instruments, and spacecraft.

  • Thermal Interface Control Documents (TICD)

    Creating and reviewing component, instrument, and observatory thermal interface control drawings and documents; publishing thermal model correlation reports and final TCS flight analysis reports.

Thermal Analysis

Service website

Full-lifecycle thermal modeling and analysis - from pre-launch through extended mission - using Thermal Desktop, TRASYS, SINDA, and CFD simulation for entire satellites, instruments, subsystems, and PCB-level components.

  • Geometric Math Model (GMM) Development
  • Analytical Thermal Math Model (TMM) Development
  • Thermal Model Correlation

    Correlating thermal models against thermal balance test results and documenting final flight predictions.

  • CFD Simulation

TCS Integration

Service website

Thermal hardware integration for spacecraft, instruments, electronic PCBs, and propulsion systems - including procurement, receiving and inspection, integration procedures, and support at launch sites and customer facilities.

  • Thermal Hardware Integration

    Hands-on integration of TCS components across spacecraft, instruments, electronic assemblies, and propulsion systems.

  • Integration Procedures Development
  • Launch Site and Customer Site Support

Test Support

Service website

Thermal Balance (TB) and Thermal Vacuum (TV) test planning, procedure development, and execution for satellites, instruments, and spacecraft components - authored to MIL-STD-1540, MIL-HDBK-340, and NASA GSFC-STD-7000.

  • Thermal Vacuum (TV) Test Planning and Support
  • Thermal Balance (TB) Test Planning and Support
  • Ground Support Equipment (GSE) Design

    Identifying GSE requirements and designing test configurations to verify proper workmanship through thermal cycling.

Industries

Aerospace · Defense · Federal · Space

Projects

Magnetospheric Multiscale (MMS) Spacecraft TCS

Space · Client: NASA

Project details

Thermal control system design, analysis, and integration for four identically built MMS spacecraft, each carrying 27 instruments with unique TCS designs. Vertex Aerospace was engaged from the conceptual design phase and completed all major milestones - SRR, PDR, CDR, PER, Thermal Model Correlation Review, and PSR - including thermal hardware integration across spacecraft, instruments, electronic PCBs, and propulsion systems.

TDRS Thermal Control Sustaining Engineering

Space · Client: NASA

Project details

Long-term thermal control system health and safety monitoring for NASA's Tracking and Data Relay Satellites across three generations: TRW TDRS 3-7 (Gen 1), Boeing TDRS 8-10 (Gen 2), and Boeing TDRS 11-13 (Gen 3), with sustained analytical support to the NASA Space Network Project Code 452 sustaining engineering team.

ILLUMA-T Thermal Design and Analysis

Space · Client: NASA

Project details

Active and passive cooling design and analysis for the Integrated LCRD Low Earth User Modem and Amplifier Terminal (ILLUMA-T) payload, including cooling design trades recognized with a NASA Exceptional Engineering Achievement Medal.

OSAM-1 Integration and Test

Space · Client: NASA

Project details

Thermal integration and test support for OSAM-1, NASA's first robotic servicing payload on a free-flying spacecraft, requiring innovative tooling and adaptive scheduling to integrate a complex multi-subsystem configuration.