APOGEE / DYNAMICS
T+ 00:00:00 UTC ON CONSOLE
DOC // FLIGHT-READINESS REVIEW
REV 17 · 2025-04-12
CLASSIFICATION · PUBLIC
PAGE 01 / 06

APOGEE DYNAMICS.

// POSITIONING STATEMENT

A space-systems engineering consultancy delivering subsystems that survive launch, vacuum, and reentry — and the reviews in between.

// MISSION COUNTER
40+ MISSIONS.
THREE DECADES OF
FLIGHT HERITAGE.
// STATUS
NOMINAL
3 ACTIVE
5 IN REVIEW
mission-control@apogee — bash 80×24
apogee@console:~$ cat ./fleet/manifest.json | grep "status:nominal"
→ 40 records returned · 28 LEO · 7 GEO · 3 lunar · 2 interplanetary
→ thermal margin: PASS · radiation tid budget: PASS · ground link: PASS
apogee@console:~$
§ 02 / MISSIONS LOG

FLIGHT MANIFEST,
REVERSE CHRONO.

RECORDS40 / 40
FIRST FLIGHT2008.11.14
LAST FLIGHT2025.03.02
SUCCESS RATE97.5%
Helios VII
M-040 · LEO SUN-SYNC
Thermal Subsystem Lead
2025.03.02
ESA / DLR
Active radiator delivered −12% mass
vs. baseline. Telemetry green at L+30.
OPEN →
A2
Arcadia 2
M-039 · LUNAR ORBIT
Flight Software · GNC
2024.10.18
NASA / JPL
Autonomous TLI burn within 0.4 m/s.
Surface imagery returned at L+11d.
OPEN →
Cirrus-X
M-038 · MEO RELAY
Radiation Hardening
2024.06.07
JAXA
TID-tolerant FPGA stack survived
3× SAA traversal. SEU rate < 1e-9.
OPEN →
Kestrel-1
M-037 · CUBESAT 12U
Ground Ops · Mission Control
2023.11.22
ESA / CSA
14-month ops with 99.2% pass
uptime. Decommissioned nominally.
OPEN →
Vantage
M-036 · GEO COMMS
Thermal · Avionics
2023.02.14
EUMETSAT
15-year design life satellite,
delivered 4 months ahead of MRR.
OPEN →
Oryx Constellation
M-031–035 · 5 SAT
Flight Software Suite
2022.08.04
PRIVATE · TELESAT
5-satellite cluster commissioning
in 73 days. Inter-sat link verified.
OPEN →
Mariner Delta
M-030 · MARS FLYBY
Radiation · Long-Range Comms
2021.07.30
NASA
Survived 211-day cruise without
SEFI events. Closest approach: 412 km.
OPEN →
SHOWING 7 / 40 — ARCHIVE 2008–2020 AVAILABLE ON REQUEST
§ 03 / CAPABILITIES

FOUR DISCIPLINES.
ONE STANDARD.

Each discipline is led by a chartered principal with a minimum of fifteen years of flight-hardware delivery. We do not subcontract critical subsystems.
CAP-01THERMAL SYSTEMS
RADIATOR PANEL · 4× PAYLOAD

Thermal Systems

Heat-pipe networks, deployable radiators, and MLI stacks engineered against the worst-case hot and cold cases of every orbit we have flown. Margin analysis traces to ECSS-E-ST-31C.

Our thermal models are correlated to flight telemetry within ±2°C on twenty-three missions. We deliver as IGES, NX, and Thermal Desktop with full uncertainty budgets.

CAP-02FLIGHT SOFTWARE
CPU IO BUS · MIL-STD-1553B

Flight Software

Real-time, partitioned flight software for GNC, ADCS, and payload management. Built on cFE/cFS heritage with our own validated drivers for LEON3, RAD750, and Vorago Cortex platforms.

Every commit runs against a 4,800-case automated FSW test bench. We deliver to DO-178C analog rigour and have never inserted a defect found post-launch.

CAP-03RADIATION HARDENING
PARTICLE FLUX · 1e7 p/cm²/s

Radiation Hardening

TID, SEE, and displacement-damage analyses for LEO, MEO, GEO, and beyond. We design shielding, derate parts, and select rad-hard, rad-tolerant, or COTS-with-mitigation stacks.

In-house TMR voting frameworks and EDAC schemes for SRAM-based FPGAs. Heritage on TID budgets from 50 krad LEO sensors to 300 krad outer-belt transponders.

CAP-04GROUND OPERATIONS
DISH · LINK · MOC

Ground Operations

Mission operations centres staffed and procedurised from LEOP through end-of-life. We write the FOPs, train the consoles, and run the shifts when you need us to.

Tooling stack: OpenC3 COSMOS, Yamcs, and bespoke flight dynamics services. 24/7 anomaly response with median time-to-recovery under 18 minutes across 200+ events.

§ 04 / FLIGHT HERITAGE

2008 → TODAY.

SCROLL → TO SCRUB THE AXIS
2008
Inception → first contract.
Apogee Dynamics founded by three former agency engineers in a converted hangar outside Toulouse. First contract: thermal review for a sun-sync earth-observation cubesat.
2008.11
M-001 · TYRO-A · LEO
2010.04
M-003 · Equinox
2012.09
M-007 · Beacon Sat
2015
First deep-space contribution.
Radiation hardening lead for a lunar-flyby technology demonstrator. Team grows to 24. Toulouse and Bristol offices linked into a single mission ops floor.
2015.02
M-014 · Selene-L1
2017.07
M-019 · Hyperion
2019.11
M-025 · Polaris-3
2025
Forty missions on console.
Helios VII delivered. Three lunar campaigns in active phase. Team now 87 engineers across four continents, with a dedicated Mars-mission practice.
2022.08
M-031 · Oryx Constellation
2024.10
M-039 · Arcadia 2
2025.03
M-040 · Helios VII
2008 2010 2012 2015 2017 2019 2022 2024 2025
§ 05 / COMMAND TEAM

SENIOR ENGINEERS
ON CONSOLE.

Combined: 412 missions of operational experience. 8 chartered engineers. 3 former agency mission directors.
ID
NAME
RANK
DISCIPLINE
MISSIONS
STATUS
E-001
Dr. Mireille Vasseur
Principal Investigator
Thermal
23 missions · 41,200 h
Active
E-002
Tomás Reyes-Holm
Lead Flight Software Engineer
Avionics
19 missions · 33,840 h
Active
E-003
Anika Beddoe
Head of Radiation Engineering
Rad-Hard
15 missions · 28,100 h
Active
E-004
Capt. Joren Halifax
Director of Mission Operations
Ground Ops
31 missions · 52,800 h
Active
E-005
Dr. Yui Nakagawa
Senior Systems Engineer
Mission Systems
17 missions · 30,400 h
On leave
§ 06 / COMMUNICATIONS

OPEN A
COMM LINK.

→ MISSION INTAKE   missions@apogee-dyn.space
→ TOULOUSE MOC   +33 5 61 00 04 12
→ BRISTOL HQ      14 Anchor Walk, BS1 5UH
© APOGEE DYNAMICS S.A.S · TOULOUSE / BRISTOL / DENVER END OF DOCUMENT · REV 17 · 2025
CASE STUDY · M-040
DOSSIER

Helios VII

A sun-synchronous earth-observation satellite for ESA / DLR. Apogee Dynamics led thermal subsystem definition from PDR through commissioning, delivering a four-panel deployable radiator architecture that reduced overall thermal hardware mass by 12 percent against the baseline study.

Critical correlation between the as-built thermal model and on-orbit telemetry was achieved within ±1.8°C across all twelve thermal zones at L+30 days, exceeding the contractual ±5°C requirement.

Subsystems
Active radiator · MLI · Heat-pipe network · Heaters
Timeline
PDR 2022.03 · CDR 2023.07 · LAUNCH 2025.03.02
Partner
ESA · DLR · Airbus DS
Outcome
Nominal · 15-year design life
MISSION IDM-040
ORBITLEO 567km
INCLINATION97.6°
MASS1,240 kg
POWER2.4 kW EOL