Neura Parse hardware / testing in progress
AER-01
NODERIQ AERA
Compact solar-assisted lighter-than-air platform
AERA is our compact, solar-assisted lighter-than-air observation platform in development and testing. Its design pairs a portable buoyant body with a small sensing unit for local observation and NODERIQ mission context.
The device and the mission
Observe an area. Keep the source in view.
AERA's design starts with portable handling, a small sensing unit and a useful view of the assigned area. Buoyancy, total mass, solar assistance and recovery must be evaluated together before defining its operating limits.
These visuals explore proposed sensing, return and service arrangements. Final geometry, components and performance remain subject to testing.
Design viewsAER-01
Proposed arrangement / under review
Connect the landscape to a defined question.
The compact platform carries a small observation unit below its buoyant body. A local water boundary, vegetation change or mapping task needs its own sensor choice, geographic reference and collection plan.
What needs validation
Review payload stability, unobstructed sensor view, location and capture timing in the actual operating envelope.
Physical design / R1
Dimensions, access and ground space.
The device, its instruments and its ground station share one dimensional plan. These are proposed design targets for engineering review, not measured product specifications.
Orthographic drawings carry the dimensions. Perspective views show the intended proportions and surroundings. The A3 set includes both devices and both ground layouts; print at 100 percent for the stated scale.
R1 / proposed physical targets
- Overall size
- 1800 × 900 × 1060 mmLength × width × height, including fins or landing feet.
- Mass allocation
- 600 gBase hardware target, including mass allowance; lift gas and buoyancy trim excluded.
- Observation module space
- 80 × 45 × 35 mmAllocated component space; sensor resolution and mapping accuracy are not set.
- Battery allocation
- 7.4 V / 0.8 Ah / 5.92 WhNominal sizing target; chemistry, protection and usable reserve need testing.
- Solar cell aperture
- 700 × 160 mmActive surface allocation; temperature, orientation and shading affect output.
- Buoyant envelope
- 1650 × 900 × 900 mmEllipsoidal sizing model; membrane shape and gas containment require qualification.
Built around access and observation.
A reinforced lightweight envelope, removable fins and a small instrument housing keep the mass budget explicit. The sensing unit remains accessible from the ground cradle. Solar film, seams, attachments and the complete loaded mass must be checked together.
Service before release.
Inspect the envelope, attachment points, instrument retention and energy state with propulsion stopped. Gas choice and handling require their own qualified process. The ground cradle is attended support; it is not an autonomous docking station.
AERA ground handling
A compact floor cradle supports preparation and recovery on a level working area. Keep the instrument accessible and plan the operator route, transport and recovery conditions for each site.
CRD-01 / ground handling
- Ground cradle
- 1200 × 700 × 650 mmAttended support for readiness checks and instrument access.
- Site allocation
- 3000 × 3000 mmA level handling area; wind, access and recovery need a site review.
- Transport case target
- 700 × 450 × 250 mmEnvelope deflated; lift-gas supply and storage are outside this allocation.
Mass, energy and the sizing assumptions
Mass budget / proposed allocation
- Envelope and seams
- 145 g
- Fins and attachments
- 50 g
- Instrument housing
- 35 g
- Propulsion and guards
- 90 g
- Sensing and navigation
- 75 g
- Battery
- 65 g
- Solar laminate
- 70 g
- Wiring and power conversion
- 35 g
- Unallocated mass allowance
- 35 g
The ellipsoidal envelope model gives 0.700 m³. At an assumed air density of 1.225 kg/m³, 15 °C and 101325 Pa, ideal helium sizing gives about 739 g of lift before the dry system. Against the 600 g allocation, the static difference is about 139 g. This difference must be resolved by measured buoyancy trim and vertical-control testing. It is not a payload rating or flight reserve: shape, leakage, temperature, pressure and measured mass can change the result. Helium is a calculation reference, not a selected product gas.
The 700 × 160 mm solar aperture gives about 24.6 W only in an ideal sizing calculation at 1000 W/m² and an assumed 22 percent cell efficiency. Curvature, angle, heat, shading and power conversion reduce useful output. The 5.92 Wh battery and measured mission load must be evaluated together.
These calculations support sizing decisions. They do not establish endurance, weather resistance, operating altitude, mapping accuracy or unattended acceptance.
Inspect the calculation record and sourcesPlanned operating routine / under test
A wider view, carried by buoyancy.
- 01
Define the observation
Select an area, sensor, monitoring question and operator-approved mission boundary.
- 02
Check platform readiness
Assess lift configuration, weather, energy and recovery conditions against the tested operating envelope.
- 03
Collect and locate
Associate each observation with position, capture time and source quality; make delayed data visible.
- 04
Review and recover
Review the returned record in mission context and follow the planned recovery and maintenance process.
Intended uses
Start with an observation worth collecting.
Mapping and satellite context
Connect local observations to a geographic reference and, where available, licensed satellite map layers. Capture time, location, source and resolution need to stay visible when comparing observations.
Useful output
A location-linked observation record to compare with the selected map source. Satellite access and mapping accuracy require their own validation.
Environmental observation
Observe defined areas over time: vegetation, water boundaries, agricultural plots or changes in a landscape. Choose and test the sensor and ground-reference method for each question before interpreting a change.
Useful output
A monitoring area, collection schedule and comparison record, with the evidence needed to review a possible change.
Timely field data
Bring useful observations into the mission while they are still relevant. Delivery depends on sensing, processing and connectivity. A lost link or an old frame must remain visible to the operator.
Useful output
Timestamped mission context with source health and explicit treatment of delayed or missing information.
Built towards NODERIQ
From an observation to a decision.
The intended connection brings device observations into NODERIQ mission context. NowFlow provides the workflow and human review layer; NeuraOS provides the edge execution foundation. Hardware integration is part of the testing work.
A map layer, a received message and a completed task are different records. Keep source time, location, freshness, operator authority and the returned outcome connected.
Environmental responsibility
Use energy with a purpose.
Solar power is part of the design direction. Responsible operation also needs a measured account of the complete device, the mission and what happens after use.
- Solar energy and storage
- Evaluate sunlight, battery storage, sensor demand and communications together. MIRA Point adds a larger solar collection surface for parked charging. Night, cloud and battery condition constrain the next mission.
- Observation with a purpose
- Choose the area, collection frequency and sensor for the question. Assess site access, noise, wildlife sensitivity and unnecessary repeat visits as part of each proposed monitoring plan.
- A measurable footprint
- Environmental responsibility includes energy use, materials, service life, maintenance, recovery and end-of-life treatment. Solar assistance is a design choice; a lower overall footprint needs lifecycle evidence.
Current development stage
Hardware tests are ongoing.
Neura Parse is developing and testing these devices for intended use with NODERIQ. The current pages describe the device direction and planned uses. Detailed operating specifications and acceptance results will follow the relevant tests.
The test programme must establish the operating envelope, observation quality, energy budget, connection recovery and return behaviour. Published results will need to support any later coverage, endurance, latency or environmental performance claim. NODERIQ integration and physical operation each require acceptance.
What the device tests must establish
- Buoyancy and gas selection
- Lift comes from gas less dense than the surrounding air. Helium and hydrogen are candidate approaches; the final choice, containment, handling and operating envelope remain subject to engineering and safety qualification.
- Solar-assisted sensing
- Solar collection supports the intended energy system. Payload demand, storage, propulsion, wind and day-to-night conditions must be evaluated together before setting an endurance claim.
- Mapping and delivery
- Retain location, capture time and sensor quality. Evaluate local processing, communication delays and recovery of retained observations after a link returns.
Technical context and sources
These sources explain buoyancy, observation, landing guidance and solar layout. They provide external engineering context; they do not verify Neura Parse hardware, establish its final design or claim a partnership or adopted software integration.