Earth launch
A commercial launcher places the compact transfer vehicle into Earth orbit.
Lunar logistics infrastructure
Space becomes
deliverable.
An autonomous platform on the lunar surface collects samples and sends them with an electromagnetic impulse — without launching a new spacecraft for every delivery.
01 / CONCEPT STAGELunar surface · 00°
SCROLL TO EXPLORE
01 / FIRST PAYLOAD
SAMPLE / LOADING
Hold and rotate · 360°
SAMPLE
LS–001
LS–001
Limited first mission
Your fragment
of another world.
Apply for a place in the early scientific and collectible lunar sample delivery programme. Final availability depends on mission success, permits and scientific verification.
Reservation deposit$100
The remaining balance is requested only after the platform becomes operational and your sample allocation is confirmed.
- Class
- Nano
- Sample mass
- 5–20 g
- Origin
- Lunar regolith
02 / MISSION ARCHITECTURE
One platform. Repeated missions.
One system.
Six mission phases.
LELP separates permanent lunar infrastructure from the payload that returns. The platform lands once, then repeats the collect–package–launch cycle.
10–25 kgplatform mass
Solar + Li-ionrechargeable power
5–1200 gMVP sample range
Lunar landing
The lander deploys LELP, solar arrays, communications and the sampling system.
Survey & collect
Cameras map local terrain while the robotic tool selects rock and regolith.
Verify & package
Material is identified, weighed, sealed in a capsule and logged for traceability.
Electromagnetic launch
Supercapacitors discharge through the launcher while the platform stays on the Moon.
Guidance & recovery
A lightweight stage corrects the trajectory toward orbit or a future return architecture.
03 / THE PLATFORM
Built to stay
Engineering
for permanent
presence.
A modular aluminium–titanium structure integrates autonomous navigation, energy storage, payload handling and electromagnetic launch.
≤50cm
MVP envelope
MVP envelope
10–25kg
platform mass
platform mass
5–1200g
MVP samples
MVP samples
04 / SYSTEMS
Inside LELP
A system designed
to repeat.
Autonomy
Flight computer, cameras, IMU and communications for remote operations.
Energy
Solar arrays, Li-ion batteries and pulse-delivery supercapacitors.
Payload handling
Manipulator, sampling tool, container and replaceable capsule magazine.
05 / ELECTROMAGNETIC LAUNCH
No combustion at liftoff
Impulse.
Silence.
Trajectory.
The linear electromagnetic launcher gives the capsule its initial velocity. A miniature electric propulsion system may correct the course, but is not used for lunar lift-off.
DEMO10–100m/s · ground validation
HOP300–500m/s · surface logistics
ORBIT800–1500m/s · with kick stage
06 / ROADMAP
From proof to infrastructure
The road to the Moon
starts in the laboratory.
Current programme maturity · Phase 0
The next logistics network
The first delivery line
beyond Earth.
Follow LELP development or request participation in the early payload programme.