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Spacecraft power

MP Space

A$23m to scale spacecraft power systems. The test is whether design selections become reliable, profitable deliveries. [1] analysis

CountryAustralia

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From component inputs to spacecraft buyer

Schematic separates input categories, manufacturing and the direct sales function.

Complete participants, relationships and sources

Cells and components

analysis

Input categories; vendors and procurement channel unverified. [6]

Schematic role; no named commercial contract is inferred.

Pack2 8S3P datasheet: page footers differ, revisions 10 and 9

Publication date not recorded; Accessed 2026-11-01

Open original source

Harwin specifications

company claim

Named connector makes in the datasheet; direct supply contract unverified. [6]

Schematic role; no named commercial contract is inferred.

Pack2 8S3P datasheet: page footers differ, revisions 10 and 9

Publication date not recorded; Accessed 2026-11-01

Open original source

MP Space manufacture

analysis

Integration and manufacturing activity described by management. [2]

Schematic role; no named commercial contract is inferred.

Manufacturing plans and management interview

Published 2026-10-27; Accessed 2026-11-01

Open original source

MP Space direct sales

analysis

Same company, separate sales function shown for clarity. [5]

Schematic role; no named commercial contract is inferred.

Spacecraft integrator or operator

analysis

Intended purchaser category, without named contracts. [5]

Schematic role; no named commercial contract is inferred.

Material: pack inputs

analysis

Cells and components → MP Space manufacture

Illustrative integration of cells, enclosure and electronics. [6]

What happens
If manufactured as specified, cells, electronics and enclosure would enter pack assembly.
Why it matters
These inputs provide storage, management and mechanical support.
What follows
Identify vendors, screening records and traceability; the procurement chain remains unconfirmed.

Illustrative relationship; amounts and contract terms are unavailable.

Pack2 8S3P datasheet: page footers differ, revisions 10 and 9

Publication date not recorded; Accessed 2026-11-01

Open original source

Dependency: specified interface

analysis

Harwin specifications → MP Space manufacture

Harwin part specifications constrain the interface; this is not a procurement assertion. [6]

What happens
Specified Harwin interfaces constrain connector selection.
Why it matters
The spacecraft harness must mate with the selected pack configuration.
What follows
If procuring these parts, verify the controlled connector revision and approved supply channel.

Illustrative relationship; amounts and contract terms are unavailable.

Pack2 8S3P datasheet: page footers differ, revisions 10 and 9

Publication date not recorded; Accessed 2026-11-01

Open original source

Material: offered packs

analysis

MP Space manufacture → MP Space direct sales

Internal product-to-sales hand-off is schematic. [5] [2]

What happens
If a pack passes manufacturing acceptance, it could enter the direct sales delivery process.
Why it matters
Accepted hardware is needed to fulfil a prospective order.
What follows
Confirm production output and customer acceptance; this internal hand-off is schematic.

Illustrative relationship; amounts and contract terms are unavailable.

Manufacturing plans and management interview

Published 2026-10-27; Accessed 2026-11-01

Open original source

Material: equipment offer

analysis

MP Space direct sales → Spacecraft integrator or operator

Proposed delivered hardware path through direct sales. [5]

What happens
If contracted and accepted, MP Space would deliver hardware to the buyer.
Why it matters
The buyer needs an integrated storage product for its spacecraft.
What follows
Check named orders, delivery records and mission configuration before claiming adoption.

Illustrative relationship; amounts and contract terms are unavailable.

Information: mission requirements

analysis

Spacecraft integrator or operator → MP Space direct sales

Product enquiries and configuration discussions precede purchase. [5]

What happens
A prospective buyer can submit mission needs through the enquiry route.
Why it matters
Configuration discussions would establish whether the product fits the mission.
What follows
If discussions proceed, document interfaces and acceptance criteria; no specific negotiation is established.

Illustrative relationship; amounts and contract terms are unavailable.

Money: purchase payment

analysis

Spacecraft integrator or operator → MP Space direct sales

Illustrative payment path; cash receipts not established. [5]

What happens
If a purchase completes, the buyer would pay through the direct sales relationship.
Why it matters
The payment would fund the agreed equipment and obligations.
What follows
Verify invoicing, terms and cash receipts; the diagram does not establish a completed transaction.

Illustrative relationship; amounts and contract terms are unavailable.

Scope. Producer and seller are functions of MP Space, not separate legal entities. No undisclosed cell vendor, distributor or named buyer is invented. Downstream service customers remain unknown.

Diagram

MP Space: charge, store and supervise

SC1 regulates solar charging; Pack2 integrates battery storage, management and heating for the host spacecraft.

Use Enlarge drawing for detail. The tour caption explains the selected elements.

MP Space: charge, store and superviseSC1 regulates solar charging. Pack2 includes storage, management and heating. Host array, computer and loads are general context; wiring is schematic.MP Space: charge, store and superviseCurrent product functions. Host interfaces are schematic.Host solar arraySunlight becomeselectrical energyPowerSC1 chargerSolar MPPTProgrammable chargingCompany product functionCharge energyPack2 integrated moduleLi-ion storageCell groupBMSSense and protectBalance cellsInternal heaters and thermal controlFunctional blocks, not a physical cutawayHost computerReceives statusCAN interfaceDashed: informationVoltage, current,temperatureHost electricaldistributionand loadsStored energyEclipse supplySolid: energyNo exact wiring, combined-system qualification or lifetime is implied.Bolay (2022) studies REIMEI ageing, not Pack2.Company evidence retrieved 1 November 2026. Independent review pending.

Step 1 of 4: 1. Regulate solar charging. Static diagram.

Guided reading, not physical motion.

Step timings allow time to read. They do not represent physical speed or duration.

  1. 1. Regulate solar charging

    The host array generates electricity. SC1 tracks the solar operating point and regulates charging. No MP Space solar-array design is implied.

  2. 2. Store energy

    Pack2 stores charge in lithium-ion cells. Its enclosure contains management electronics and thermal-control functions.

  3. 3. Supervise and report

    The integrated BMS supervises cell limits and balancing. Internal heaters support thermal control. CAN carries battery status to the host; supervision is continuous, not a later event.

  4. 4. Supply spacecraft loads

    Stored energy supports the host electrical system when solar generation is unavailable. The functional arrow omits mission-specific switching and regulation.

Read left to right from the host solar array to SC1 charge control, then down to the Pack2 boundary containing storage, BMS and heating. A separate energy path connects storage to host distribution and loads. A dashed path represents CAN status information to the host flight computer. Solid arrows denote energy; dashed arrows denote information. Functions are shown without physical scale or measured timing.

Sources. [5] [11] [6] [8] [12]

Limitations.

  • Company product functions, not a reference circuit or verified combined system. No current rating, efficiency, chemistry, cell count, dimensions or usable orbital energy is inferred. SC1 compatibility, switching, return paths and power-distribution hardware require a mission design. The 8S3P PDF has inconsistent revision footers. Ground qualification reports and independent orbital performance are unavailable. REIMEI is a different battery system. Independent source and rendered reviews remain pending.
Evidence
  • company claim. Pack2 integrates storage, management and thermal-control functions. [6] [5]
  • company claim. SC1 provides solar MPPT and programmable charge regulation. [11]
  • analysis. The spacecraft generation, distribution and computing blocks provide general functional context. [12] [6]
  • analysis. Functional placement does not establish mission wiring, qualification or lifetime. REIMEI ageing research cannot validate Pack2. [6] [8]

Diagram elements

  • context: explanatory simplification. Title and scope show a functional product explanation, not a circuit. Pages 1-2 [6] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • array: explanatory simplification. Generic host solar generation, not an MP Space array. Photovoltaics [12] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • solar-power: explanatory simplification. Electrical input from array to charger. SC1 introduction [11] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • charger: explanatory simplification. MPPT and programmable battery charge function. SC1 introduction and feature list [11] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • charge: explanatory simplification. Charge energy to storage, functional not circuit topology. SC1 introduction [11] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • pack-boundary: explanatory simplification. Pack2 boundary contains storage, BMS and heating. Page 1, integrated pack and BMS features [6] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • cells: explanatory simplification. Symbolic storage block; no chemistry, cell count or wiring specified. Page 1, product render [6] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • bms: explanatory simplification. Management senses state, balances cells and protects limits. Page 2, protection and telemetry feature rows [6] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • heater: explanatory simplification. Internal heating function; no heat-transfer rate shown. Pages 1-2, heaters and thermal control [6] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • computer: explanatory simplification. Host flight computer shown as receiver of battery status. Page 1, CAN 2.0; page 2 telemetry [6] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • telemetry: explanatory simplification. Dashed information path for voltage/current/temperature status. Page 2, communication and telemetry [6] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • load: explanatory simplification. Host distribution and load block, without converters or switches specified. Electrical Power Distribution and Storage [12] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • discharge: explanatory simplification. Stored energy serves spacecraft loads when solar supply is unavailable. Electrical Power Storage [12] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.
  • caveat: explanatory simplification. Ageing model and company evidence limitations remain visible. Figure 3 and section 5.1 [8] Limitation. Functional schematic only. Shape, placement and arrows are not a measured or complete electrical design.

Interactive 3D explainer

Inside a spacecraft battery

Cells store electrical energy. Protection, heating and interfaces make that energy usable by the spacecraft.

The static explanation below is available without 3D or JavaScript.

Evidence boundary. Teaching reconstruction from MP Space drawings. CAD, website and drawing revisions differ. Reveals are not operating motion; no wiring or performance simulation.

Static explanation and all component roles
  1. Closed pack: a stationary explanatory view, not measured motion.
  2. Inside the pack: a stationary explanatory view, not measured motion.
  3. Enlarged thermal section: a stationary explanatory view, not measured motion.
  4. Separate the parts: a stationary explanatory view, not measured motion.
Cover and cell supports
Endplates, cover and nylon clamshells hold the cell array and side board.

Purpose. They locate and protect the components as one mountable pack.

Observed topology reconstructed; tolerances and the current approved revision are not established.

company claim | inspected 2026-11-01 | Source 1 | Source 2

24 storage cells
Three rows of eight cylindrical cells store and release electrical energy.

Purpose. The cells provide stored energy when the spacecraft needs it.

No internal chemistry, busbar route, charge rate or state of charge is depicted.

company claim | inspected 2026-11-01 | Source 1 | Source 2

Battery management board
The side board monitors battery state and provides balancing and protection.

Purpose. Cells need management within their operating limits.

Board location is sourced. Component circuitry and hidden connections are deliberately omitted.

company claim | inspected 2026-11-01 | Source 1 | Source 2

Heaters and heat paths
Annular heaters sit at cell ends. A spreader and BMS strap provide thermal paths.

Purpose. Cold cells need warming; heat must also reach the spacecraft interface.

The thermal section is enlarged and layer separation is explanatory. Gap-pad design is customer-defined; no temperature or heat-flow rate is simulated.

company claim | inspected 2026-11-01 | Source 1 | Source 2

Power and signal ports
One end carries power and two signal ports. Auxiliary power is at the opposite end.

Purpose. The spacecraft needs both energy transfer and battery information.

Connector positions follow the drawing. Pinout and actual spacecraft harness are not shown.

company claim | inspected 2026-11-01 | Source 1 | Source 2

External charging role
A separate charge controller manages energy arriving from a solar supply.

Purpose. Solar input must be controlled before charging the cells.

SC1 is a separate product. This context arrow is not a verified SC1-to-Pack2 wiring design.

company claim | inspected 2026-11-01 | Source 1

company claim; analysis geometry · MP Space source. Source inspection dates are listed for each component. Publication date is recorded in the dossier source list where established. Every shape is an explanatory simplification; the scene does not establish engineering performance.

Capital, customers and market direction

Money and market

Evidence checked to . Company finances and wider-market indicators are kept separate.

Announced seed round

AUD 23m

MP Space says it closed financing to expand manufacturing, product platforms and the engineering team. [F1]

The USD translation is the same round, not additional capital. Cash receipt and dilution were not inspected.

company claim

Commercial pipeline

500+ spacecraft

The company reports design selection across more than 500 spacecraft. [F1]

Design-ins are not accepted shipments, non-cancellable backlog or recognised revenue.

company claim

Battery-sector signal

USD 935.6m

EnerSys reported Q1 fiscal 2027 sales, up 4.8% from USD 893.0m. Its release attributes only about 1% to organic volume. [F2]

Group results span industrial markets. The fiscal quarter ended 5 July 2026; it is not a calendar-2027 forecast.

verified

Cash and runway

Not disclosed

Not established. Current cash, committed facilities, monthly cash burn and a funded milestone plan have not been obtained.

A financing announcement is not the cash balance. No runway estimate is shown.

analysis

What the market signal means

Turn design wins into cash-generating production

The immediate test is conversion of design selections into qualified deliveries. EnerSys shows why sales growth needs decomposition: pricing and currency can lift revenue without equivalent volume growth. [F1] [F2]

No competitor cost curve or price per Wh is transferable to MP Space without matched mission requirements.

analysis

EnerSys quarterly net sales

First fiscal quarter in successive years.

USD million. Bars start at zero.

Q1 FY2026893
Q1 FY2027935.6

Industrial battery group context; not an ABSL-only series or MP Space forecast. [F2]

Source location: Key Financial Results, Net Sales, June 29 2025 and July 5 2026. Reported values; no forecast or startup valuation.

Questions that change the financial case

  • How many selected spacecraft have signed quantities, deposits and acceptance dates?
  • What cash is tied up in cell screening, inventory, qualification and customer receivables?
  • What is gross margin per qualified pack after yield, warranty and engineering support?
Financial overview sources and dates
  1. F1 MP Space seed financing and design selections

    Published 2026-10-26 · Accessed 2026-11-01

  2. F2 EnerSys Q1 fiscal 2027 results

    Published 2026-08-12 · Accessed 2026-11-01

The development

The earliest located report timestamp is 25 October at 19:04 UTC in Forbes metadata; its visible date is 26 October. MP Space announced the A$23m seed round on 26 October. Blackbird led it; manufacturing expansion is planned, not achieved output. [1] [3] analysis

Claims and evidence

  • A$23m to scale spacecraft power systems. The test is whether design selections become reliable, profitable deliveries. [1]

    analysis
  • The earliest located report timestamp is 25 October at 19:04 UTC in Forbes metadata; its visible date is 26 October. MP Space announced the A$23m seed round on 26 October. Blackbird led it; manufacturing expansion is planned, not achieved output. [1] [3]

    analysis
  • The Australian register records MP SPACE PTY LTD as an active Australian private company. The current cap table was not obtained. [4]

    verified
  • The company reports design selections covering more than 500 spacecraft. This is not evidence of delivered units, recognised revenue or non-cancellable backlog. [1]

    company claim
  • Flight-heritage wording differs between sources. Payload reports a first launch with an unnamed customer; successful in-orbit operation remains unverified. [1] [2]

    analysis
  • Current specifications list 432 Wh and 2.4 kg for 8S3P, and 864 Wh and 4.5 kg for 8S6P. Energy is nameplate at 23 degrees C, not usable orbital energy. [5] [6] [7]

    company claim
  • A published study modelled degradation in a different satellite battery system, REIMEI. It highlights why cycling conditions and ageing mechanisms matter, but does not validate MP Space products. [8]

    analysis

Assessment

TopicReading and evidence
Product and mechanismIntegrated lithium-ion packs and battery management are the starting product. Cell chemistry alone cannot establish pack reliability. [5]

analysis

Customers and buying processConstellation operators can buy a qualified subsystem or build it internally. Qualification duration, integration support and failure responsibility may determine the buying decision. [2]

analysis

Commercial proofDesign selections are encouraging, but contracts, customer acceptance and revenue recognition are unavailable. Treat the scale claim as a pipeline indicator. [1] [2]

analysis

Pricing or economicsManagement describes a cost advantage in an interview. No comparable quotation, costed bill of materials or audited margin bridge was obtained. [2]

analysis

Competitors and substitutesThe central alternative is an operator's own engineering team or an established subsystem supplier. A price comparison must include qualification and integration costs. [2]

analysis

DistributionDirect constellation relationships could support repeat orders. Evidence of channel economics, concentration and repeat purchase rates is missing. [1]

analysis

Intellectual property or defensibilityNot established. Obtain patent ownership, software ownership, supplier exclusivity and evidence that qualification history protects margins.

unknown

Manufacturing or operational scalingCapital can fund tooling and engineering. Throughput, first-pass yield, rework, test duration and accepted deliveries would test whether scale reduces cost. [1] [2]

analysis

RegulationNot established. Obtain applicable export classifications, launch-provider requirements and customer-specific qualification and acceptance records.

unknown

Capital needsThe round amount does not reveal runway. Inventory financing, equipment spending, hiring and customer payment terms determine the next capital requirement. [1]

analysis

Key risksQualification claims lack underlying reports. Pack ageing depends on operating conditions; research on another battery cannot fill this evidence gap. [6] [7] [8]

analysis

Next falsifiable milestoneNamed customer acceptance with repeat deliveries, a reconciled flight record and production yield data would strengthen the case. Persistent rework or cancelled designs would weaken it. [1] [2]

analysis

TeamOriginal reporting describes founders with automotive battery experience. Relevant experience helps the transfer thesis, but is not evidence of space qualification or manufacturing execution. [3]

analysis

Public-market contextEnerSys provides product-category context through its ABSL space batteries. Its group financials do not isolate ABSL or establish MP Space margins, capital needs or valuation. A seed amount is not a company valuation. [9] [10]

analysis

Two pack sizes, different nameplate energy

Scale: 0 to 864 Wh at 23 degrees C

8S3P: 432 Wh at 23 degrees C

8S6P: 864 Wh at 23 degrees C

Current company specifications. These are nominal pack values, not independently measured usable energy. Limits. Different pack masses and sizes. This is not a ranking of energy density, lifetime or reliability. Publication dates are unresolved; sources retrieved 1 November 2026.
Reported values
ItemValue (Wh at 23 degrees C)Date and evidence
8S3P432undated
company claim [6]
8S6P864undated
company claim [7]

Opinion

The interesting bet is a repeatable subsystem business, rather than a new battery chemistry. Standard products could spread engineering and qualification cost across customers. I would watch accepted repeat deliveries and production yield before drawing conclusions from design selections.

Limits. This is a research view, not a valuation. Ownership, contracts, margins and independent flight performance remain unresolved. A failed qualification or poor repeat-order conversion would challenge the thesis.

opinion

Commercial picture · 2026-11-01

Competition, costs and demand

Product and commercial context as of 1 November 2026. Unavailable evidence is identified explicitly.

Financing, product offer and buying decision

Schematic of the disclosed financing and proposed direct product business.

Complete participants, relationships and sources

Seed investors

company claim

Blackbird-led financing announced by the company. [1]

Schematic role; no named commercial contract is inferred.

MP Space

analysis

Develops and offers spacecraft power products. [5]

Schematic role; no named commercial contract is inferred.

Spacecraft buyer

analysis

Intended constellation or integration buyer. [5]

Schematic role; no named commercial contract is inferred.

Mission acceptance

analysis

Customer-specific interface and qualification decision. [6]

Schematic role; no named commercial contract is inferred.

Pack2 8S3P datasheet: page footers differ, revisions 10 and 9

Publication date not recorded; Accessed 2026-11-01

Open original source

Money: seed capital

company claim

Seed investors → MP Space

Announced financing supports expansion. [1]

What happens
Investors provide the announced seed financing.
Why it matters
MP Space says expansion and engineering require capital.
What follows
Check cash receipt, instrument terms and funded milestones.

Illustrative relationship; amounts and contract terms are unavailable.

Material: power products

analysis

MP Space → Spacecraft buyer

Direct hardware offer, not evidence of a named delivery. [5]

What happens
If a buyer selects a product, MP Space would supply the agreed hardware.
Why it matters
The intended buyer needs spacecraft energy storage.
What follows
Confirm interfaces, qualification scope and delivery acceptance before treating an offer as revenue.

Illustrative relationship; amounts and contract terms are unavailable.

Money: potential purchase

analysis

Spacecraft buyer → MP Space

Illustrative payment in a direct equipment sale. [5]

What happens
If a direct sale closes, the buyer would pay MP Space under agreed terms.
Why it matters
Payment would compensate hardware manufacture and agreed services.
What follows
Obtain payment milestones and receipts; neither is established here.

Illustrative relationship; amounts and contract terms are unavailable.

Dependency: mission fit

analysis

Mission acceptance → Spacecraft buyer

Integration requires reconciling operating and interface limits. [6]

What happens
If shortlisted, the pack would undergo customer mission-fit assessment.
Why it matters
Electrical, thermal and mechanical limits must suit the spacecraft.
What follows
Reconcile the controlled configuration and qualification reports before purchase acceptance.

Illustrative relationship; amounts and contract terms are unavailable.

Pack2 8S3P datasheet: page footers differ, revisions 10 and 9

Publication date not recorded; Accessed 2026-11-01

Open original source

Scope. No sales value, conversion rate, accepted backlog or investor instrument split is shown.

Competition and substitutes

Evidence and open questions for competition and substitutes.

TopicEvidence and scope
EnerSys ABSL

ABSL markets lithium-ion spacecraft batteries, including an 8s3p product. This is a direct product-category alternative. [9]

company claim

An identical configuration label does not imply equal cells, usable energy, qualification or price.

Epsilor

Epsilor describes satellite battery development using commercial lithium-ion cells. It is a relevant alternative approach. [13]

company claim

Undated history page; current delivery capacity and qualification status need checking.

Internal build or delayed redesign

Management identifies in-house engineering as a substitute. Retaining an existing qualified pack may avoid redesign work. [2]

analysis

Retention is an adoption hypothesis, not a measured switching rate.

Comparative funding

Not established. Competitor programme funding, recent private equity rounds and matched development budgets were not obtained. Public-group finances are shown separately.

Not established

Unavailable in the sources inspected.

Funding and capital requirements

Evidence and open questions for funding and capital requirements.

TopicEvidence and scope
Seed announcement, 26 October 2026

MP Space announced an A$23m seed round led by Blackbird, with Seraphim Space, Systemiq Capital, Speedinvest and MFV Partners. [1]

company claim

Announced closed financing; instrument terms, bank receipts and dilution were not inspected. Do not add US-dollar translations as separate capital.

Use of proceeds

Manufacturing expansion and engineering recruitment are stated uses. [1]

company claim

Plans are not commissioned capacity or cash expenditure.

Debt, grants and runway

Not established. A reconciled cash balance, debt schedule, grant receipts, burn rate and investor instrument breakdown were not obtained.

Not established

Unavailable in the sources inspected.

Costs and operating economics

Evidence and open questions for costs and operating economics.

TopicEvidence and scope
Price claim

The founder describes pricing below incumbent alternatives. [2]

company claim

No matched quotation, mission specification or fully loaded cost bridge supports a numerical discount here.

Pack and customer benchmark

Not established. Comparable 2026 Australian-dollar prices for qualified delivered packs, integration, acceptance testing and warranty were not obtained. No price per Wh is inferred from terrestrial batteries.

Not established

Unavailable in the sources inspected.

Factory and working capital

Not established. Equipment cost, capacity, yield, labour, cell screening, inventory days and customer payment terms were not obtained. CAPEX, OPEX and working capital remain separate unknowns.

Not established

Unavailable in the sources inspected.

Listed-company context

EnerSys reports consolidated costs and capital spending, but these span many industrial battery markets. [10]

analysis

No allocation to ABSL or transfer to a Sydney startup is defensible. See the separately scoped financial series.

Inputs, manufacture and distribution

Evidence and open questions for inputs, manufacture and distribution.

TopicEvidence and scope
Specified components

The 8S3P datasheet identifies Harwin power and signal connectors and an aluminium enclosure. [6]

company claim

A specified manufacturer is not evidence of a direct purchase contract or exclusive supplier.

Cell and electronics vendors

Not established. The cell manufacturer, chemistry formulation, board assembler, semiconductor vendors, procurement channel and second sources were not established.

Not established

Unavailable in the sources inspected.

Producer and seller

MP Space presents integrated products and a direct enquiry route; management describes local manufacturing expansion. [5] [2]

analysis

No distributor, contract manufacturer, sales commission or named customer relationship is inferred.

Potential growth drivers

Evidence and open questions for potential growth drivers.

TopicEvidence and scope
Product range

SC1 adds solar charge control to the storage offer. [11]

company claim

A catalogue listing does not establish shipment volume or compatibility of every configuration.

Standardisation

A repeatable pack could spread integration effort over multiple spacecraft designs. [5]

analysis

Savings depend on qualification reuse and accepted volume; neither is quantified.

Power continuity

Spacecraft loads need power when solar generation is unavailable. Storage therefore serves a clear physical requirement. [12]

verified

This establishes function, not addressable market size.

Technical and commercial blockers

Evidence and open questions for technical and commercial blockers.

TopicEvidence and scope
Mission qualification

Environmental limits and protection functions are company specifications. Underlying qualification reports and test configuration traceability remain missing. [6]

analysis

Radiation tolerance wording alone is not complete mission assurance.

Ageing and operating conditions

The REIMEI study shows why cycling conditions and model limits matter to lifetime assessment. [8]

analysis

Different cells and mission. No MP Space life or degradation curve is inferred.

Source inconsistency

The downloaded 8S3P document labels page one revision 10 and page two revision 9. [6]

verified

Supplier must reconcile the controlled revision before reliance on all details.

Production constraints

Not established. Yield, accepted monthly output, bottleneck test duration, export classifications and liability allocation remain unresolved.

Not established

Unavailable in the sources inspected.

Demand and evidence of adoption

Evidence and open questions for demand and evidence of adoption.

TopicEvidence and scope
Design selections

The company reports selection across more than 500 spacecraft. [1]

company claim

Selections are not accepted shipments, cash receipts or non-cancellable backlog.

Launch evidence

Payload reports a first launch with an unnamed customer on Bandwagon-5. [2]

analysis

Launch reporting does not establish successful sustained orbital operation.

Buyer appetite and public acceptance

Not established. Named paid deliveries, repeat-order conversion, procurement surveys and relevant public-attitude evidence were not obtained. Press attention and investor funding are not demand measurements.

Not established

Unavailable in the sources inspected.

Users, buyers and payers

Evidence and open questions for users, buyers and payers.

TopicEvidence and scope
Intended buyer

The catalogue targets constellation operators. Spacecraft integrators must assess interfaces and mission suitability. [5]

analysis

The contracting entity and budget owner are not named.

Route to purchase

The published sales route is a direct product enquiry. [5]

verified

No reseller or distribution agreement is established.

Downstream chain

Not established. Named operators, service customers, end users, purchase terms and who ultimately bears mission failure costs were not established.

Not established

Unavailable in the sources inspected.

Acquisition thesis

Not established. No acquisition discussions or strategic buyer interest were established.

Not established

Unavailable in the sources inspected.

Public-company context · 2026-11-01

Listed companies around this market

Listed battery competitor context, selected for product relevance. No valuation or share-price inference.

A listed company's share price reflects its whole business. It does not establish demand for this startup, a supplier relationship or a private valuation.

EnerSys

Competitor · analysis

Its ABSL range competes in spacecraft lithium-ion batteries. The current official results release identifies NYSE: ENS. [9] [10]

Consolidated industrial battery group; ABSL revenue, capital intensity and margins are not isolated. No MP Space supply or customer relationship is established.

View EnerSys on TradingView. External price data may be delayed or unavailable; filing evidence is shown below.

Net sales

EnerSys consolidated US GAAP net sales; twelve-month fiscal years, reported in millions. Units: USD million.

Net sales, USD million. Exact values and citations follow in the table.3,751.403,617.620252025-03-31: 3,617.6 USD million3,751.420262026-03-31: 3,751.4 USD million
PeriodReported valueFiling and evidence
2024-04-01 to 2025-03-313,617.6 USD million2026-05-21 · verified
Consolidated Condensed Statements of Income (Unaudited), twelve months ended March 31, 2025, Net sales row; USD millions [10]
2025-04-01 to 2026-03-313,751.4 USD million2026-05-21 · verified
Consolidated Condensed Statements of Income (Unaudited), twelve months ended March 31, 2026, Net sales row; USD millions [10]

Unaudited results-release table. Diversified group, not ABSL standalone economics.

Gross profit

EnerSys consolidated US GAAP gross profit; twelve-month fiscal years, reported in millions. Units: USD million.

Gross profit, USD million. Exact values and citations follow in the table.1,097.601,092.420252025-03-31: 1,092.4 USD million1,097.620262026-03-31: 1,097.6 USD million
PeriodReported valueFiling and evidence
2024-04-01 to 2025-03-311,092.4 USD million2026-05-21 · verified
Consolidated Condensed Statements of Income (Unaudited), twelve months ended March 31, 2025, Gross profit row; USD millions [10]
2025-04-01 to 2026-03-311,097.6 USD million2026-05-21 · verified
Consolidated Condensed Statements of Income (Unaudited), twelve months ended March 31, 2026, Gross profit row; USD millions [10]

Unaudited results-release table. Diversified group, not ABSL standalone economics.

Calculated comparisons

FY2025 gross profit / net sales: 30.2% analysis · calculated, rounded to 2 decimal places

100 × 1,092.4 ÷ 3,617.6. Gross profit / Net sales, period ending 2025-03-31. [10]

Derived from rounded reported inputs; group gross margin includes manufacturing tax-credit effects and does not estimate MP Space margin.

FY2026 gross profit / net sales: 29.26% analysis · calculated, rounded to 2 decimal places

100 × 1,097.6 ÷ 3,751.4. Gross profit / Net sales, period ending 2026-03-31. [10]

Derived from rounded reported inputs; group gross margin includes manufacturing tax-credit effects and does not estimate MP Space margin.

Competitive landscape · 2026-11-01

Who else solves this?

Space-qualified battery cells, packs and integrated small-satellite storage.

Comparison lens. MP Space competes against mission-qualified suppliers as well as standard small-satellite packs. Useful comparison requires usable energy at end of life, mass, temperature range, radiation environment, charge control and qualification scope. analysis

Established supplier · United Kingdom and United States

EnerSys ABSL

Lithium-ion space batteries in mission-specific configurations.

Difference
A qualified-supplier procurement alternative; compare the exact pack and mission environment with MP Space.
Maturity
Established space battery product portfolio with configuration-specific offerings.
Economics
Programme quotations and integration cost are not published on the product page.
Funding / ownership
ABSL is offered within EnerSys; product-specific development funding is not disclosed.

Heritage across a product family is not qualification evidence for an arbitrary new configuration.

analysis

Sources and dates

EnerSys ABSL space batteries (published date not stated; accessed 2026-11-01)

Established supplier · France and United States

Saft

Space cells and battery systems serving multiple orbital applications.

Difference
A cell-to-pack supplier across larger mission classes; scale and test scope may differ substantially from an MP Space small-satellite product.
Maturity
Named supply for EUMETSAT third-generation weather satellites accompanies the current space portfolio.
Economics
No directly comparable delivered-pack quote or lifecycle cost is disclosed.
Funding / ownership
Saft identifies itself as a TotalEnergies subsidiary in its 2023 mission announcement; battery-line funding is not stated.

A large weather-satellite reference is not a like-for-like small-satellite cost benchmark.

analysis

Sources and dates

Saft space battery portfolio (published date not stated; accessed 2026-11-01) · Saft EUMETSAT supply and ownership (published 2023-03-09; accessed 2026-11-01)

Direct competitor · Denmark

GomSpace NanoPower BPX

A standard small-satellite battery pack with telemetry, thermal control and modular integration.

Difference
A catalogue-pack alternative; compare usable energy and interfaces with MP Space rather than cell-level energy density.
Maturity
Current product page markets the BPX pack and describes flight-tested technology.
Economics
A project-specific quote is required; no comparable public delivered price was established.
Funding / ownership
GomSpace product programme; pack-specific investment and funding are not disclosed in this source.

Advertised nominal energy is not automatically usable end-of-life energy; qualification of the required variant remains essential.

analysis

Sources and dates

GomSpace NanoPower BPX (published date not stated; accessed 2026-11-01)

Established supplier · Israel

Epsilor

Custom battery development for space applications, including satellite battery programmes.

Difference
A custom-engineering alternative where pack design and mission qualification are bought together.
Maturity
Company history describes space battery work; the historical record does not establish current delivery capacity.
Economics
Custom quotation, qualification cost and replacement economics are unknown.
Funding / ownership
Current ownership and programme funding were not established from this history page.

Historical satellite participation is a capability signal, not a current product qualification or availability guarantee.

analysis

Sources and dates

Epsilor space battery history (published date not stated; accessed 2026-11-01)

Coverage limits. Four named supply options span different spacecraft sizes. No common qualification test, pack-level end-of-life energy dataset, delivered pricing or independently verified market share is available. Supplier heritage cannot be transferred automatically to a new cell or pack.

Sources

  1. 1
    Seed financing announcement

    company | Published 2026-10-26 | Accessed 2026-11-01

  2. 2
    Manufacturing plans and founder interview

    independent reporting | Published 2026-10-27 | Accessed 2026-11-01

  3. 3
    Financing and earlier pitch: UTC metadata 25 October, visible date 26 October

    independent reporting | Published 2026-10-25 | Accessed 2026-11-01

  4. 4
    Australian Business Register: MP SPACE PTY LTD

    registry | Published undated | Accessed 2026-11-01

  5. 5
    Current product specifications

    company | Published undated | Accessed 2026-11-01

  6. 6
    8S3P revision 10 datasheet; publication date unresolved

    company datasheet | Published undated | Accessed 2026-11-01

  7. 7
    8S6P revision 12 datasheet; publication date unresolved

    company datasheet | Published undated | Accessed 2026-11-01

  8. 8
    Bolay et al.: satellite battery degradation; author manuscript

    journal paper author manuscript | Published 2022-02-04 | Accessed 2026-11-01

  9. 9
    EnerSys ABSL spacecraft battery catalogue

    company | Published undated | Accessed 2026-11-01

  10. 10
    EnerSys corrected fiscal 2026 results and financial statements

    company financial statements | Published 2026-05-21 | Accessed 2026-11-01

  11. 11
    SC1 solar charger and MPPT

    company | Published undated | Accessed 2026-11-01

  12. 12
    NASA: electrical power generation, distribution and storage

    official technical manual | Published undated | Accessed 2026-11-01

  13. 13
    Epsilor satellite battery development

    company | Published undated | Accessed 2026-11-01