02 / Selected work
Systems in practice.
Selected initiatives spanning reliability, applied AI, release engineering, aerospace, and independent product development.
01 / RELIABILITYDell Technologies
SRE dashboard &
monitoring platform
A full-stack platform that brings infrastructure telemetry into one engineering workflow, replacing scattered manual checks.
CONTRIBUTIONCarried the platform from idea to production. Built telemetry collection across 100+ Jenkins controllers and optimized dashboard queries to stay under one second.
AngularFastAPIRedisElasticsearch
02 / APPLIED AIDell Technologies
MCP integrations
for SRE
Tool interfaces that let an LLM support infrastructure operations, with an engineer reviewing every action.
CONTRIBUTIONBuilt integrations used daily by the SRE team, connecting AI tooling to operational workflows.
MCPLLM toolingPython
03 / ENGOPSDell Technologies
Release provisioning
automation
Automated release-branch provisioning for high-priority enterprise clients, addressing delays identified with release and product teams.
RESULTReduced delivery time from two days to three hours.
AutomationRelease engineering
04 / PERSONALIndependent
SoTravel
trip-planning app
A collaborative app for coordinating group trips, built solo from idea to shipped product.
CONTRIBUTIONOwned the full stack — authentication, trip creation, invitations, and join flows — resolving SDK, routing, and data-contract issues along the way.
ExpoSupabaseSQLApple Sign-In
05 / AEROSPACESTAR · UC Berkeley
CALDERA
two-stage supersonic rocket
As Recovery Lead, led recovery systems for a two-stage rocket reaching supersonic speeds under tight design constraints.
CONTRIBUTIONDeveloped flight profile analysis to define the parameters for a successful staged flight sequence using commercial-off-the-shelf hardware.
Recovery systemsFlight profile analysisStaged flight
06 / AEROSPACESTAR · UC Berkeley
ALULA
liquid-engine rocket recovery
As Recovery Lead, coordinated the engineering team tackling recovery of a liquid-engine rocket.
CONTRIBUTIONDeveloped an Instron failure-load test to quantify recovery-hardware failure points. Designed a Y-harness that prevented parachute deployment loads from tearing the airframe — a failure known as zippering — enabling a successful recovery.
Liquid-engine recoveryFailure-load testingStructural design
07 / AEROSPACESTAR · UC Berkeley
MINDI
Mach 2 & a campus apogee record
Contributed to recovery and design as a member of the 20-person team behind a rocket with a 54 mm internal diameter. MINDI reached Mach 2 and set UC Berkeley’s campus apogee record at approximately 28,000 ft.
CONTRIBUTIONWhen the team discovered a center-of-pressure stability problem at the launch site, proposed the corrective design the team adopted under schedule pressure, enabling a successful flight.
Minimum-diameter designFlight stabilityProblem-solving under pressure