2 INFINITY LOGISTICS LLP
Developing electromagnetic launchers to reduce the cost and environmental impact of space payload launches.
Cover Block
Public sources
| Field | Value |
|---|---|
| Name | 2 INFINITY LOGISTICS LLP |
| Tagline | Developing electromagnetic launchers to reduce the cost and environmental impact of space payload launches. [Kerala Startup Mission, September 2025] |
| Headquarters | Alappuzha, India [Tofler, May 2025] |
| Founded | 2023 [Tofler, May 2025] |
| Stage | Pre-Seed |
| Industry | Deeptech |
| Technology | Space |
| Geography | South Asia |
| Founding Team | Co-Founders (2): Thazhamtharayil Selvarajan Sandeep, Swathi Thazhantharayil Selvarajan [Tofler, May 2025] |
| Funding Label | Pre-seed |
Links
Public sources
Executive Summary
PUBLIC 2 INFINITY LOGISTICS LLP is a Kerala-based space technology startup pursuing electromagnetic launchers as a lower-cost, lower-emissions path to putting payloads into space, which is enough to merit early investor attention because the technical ambition is large while the public company footprint is still unusually early [Kerala Startup Mission, September 2025] [Tofler, May 2025]. The company was incorporated as an LLP on September 15, 2023 in Alappuzha, India, and its public profile remains concentrated in registration records, a Kerala Startup Mission startup listing, and LinkedIn references rather than reported commercial milestones [Tofler, May 2025] [Kerala Startup Mission, September 2025].
The core proposition is straightforward: use electromagnetic launch systems to reduce launch cost and environmental impact, with public descriptions referring to cargo delivery in space and technical literature showing that electromagnetic launcher concepts have long been studied for payload classes from roughly 100 kg to 1000 kg and exit velocities in the 4 to 6 km/s range [Kerala Startup Mission, September 2025] [LinkedIn, October 2026] [UNT Digital Library] [NASA Technical Reports Server (NTRS), 1985]. That said, the available evidence does not yet establish a demonstrated product, launch timetable, customer base, or regulatory path, so the differentiation is still more conceptual than commercially proven on the public record [Kerala Startup Mission, September 2025] [LinkedIn, October 2026].
On team, public corporate records identify Thazhamtharayil Selvarajan Sandeep and Swathi Thazhantharayil Selvarajan as designated partners, while LinkedIn evidence associates Sandeep T. S. with the founder and CEO role and links him to IIT Guwahati and Carnegie Mellon University [Tofler, May 2025] [LinkedIn, retrieved 2026]. The financing picture is similarly early: no confirmed venture round or named investor appears in the sourced material, Kerala Startup Mission is the only documented institutional affiliation, and Tofler lists LLP capital contribution at ₹0.10 lakh, which indicates that investors should treat the company as pre-seed and pre-institutional until better evidence emerges [Kerala Startup Mission, September 2025] [Tofler, May 2025].
Over the next 12 to 18 months, the key watchpoints are whether the company can move from directory-level presence to evidence of technical validation, external funding, and a clearly defined buyer set, likely among payload operators if the concept matures, although that customer mapping remains an inference rather than a verified go-to-market plan [Kerala Startup Mission, September 2025] [Tofler, May 2025]. For now, the case rests on an ambitious deeptech thesis with limited public proof points, which is often where outlier outcomes begin but also where diligence needs to stay disciplined.
Company-stated, unverified -- This section relies materially on company or directory-style sources, with technical context corroborated by NASA and UNT but operating claims still largely unconfirmed.
Taxonomy Snapshot
| Axis | Value |
|---|---|
| Stage | Pre-seed |
| Industry / Vertical | Deeptech |
| Technology Type | Space |
| Geography | South Asia |
| Founding Team | Co-Founders (2) |
| Funding | Pre-seed |
How the Company Got Here
PUBLIC
The public record on 2 INFINITY LOGISTICS LLP is thin, but what is clear is that this is a newly incorporated Indian space-technology entity rather than a conventional freight operator. Tofler lists the business as an LLP incorporated on 15 September 2023 in Alappuzha, Kerala, with its registered location in the Chengannur area, and names Thazhamtharayil Selvarajan Sandeep and Swathi Thazhantharayil Selvarajan as designated partners [Tofler, May 2025].
The company’s most specific public description comes from Kerala Startup Mission, which lists 2 INFINITY LOGISTICS LLP as a certified startup and says its proposition is to reduce the cost and environmental impact of sending payloads to space [Kerala Startup Mission, September 2025]. That framing aligns with the company’s limited public footprint as a deeptech venture formed in 2023, though the available sources do not establish a commercial launch, customer deployment, or outside financing event [Kerala Startup Mission, September 2025] [Tofler, May 2025].
Chronology is straightforward from the documents that are available. The LLP was incorporated in September 2023 [Tofler, May 2025], and by September 2025 it appeared on Kerala Startup Mission’s platform as a certified startup with an electromagnetic-launcher based proposition [Kerala Startup Mission, September 2025]. Tofler reports LLP capital contribution of ₹0.10 lakh, which indicates a very early formal capitalization base, although that figure should not be read as venture funding [Tofler, May 2025].
Lightly corroborated -- Confirmed by Tofler and Kerala Startup Mission, with chronology and legal-entity details resting primarily on directory and institutional listings.
Product and Technology
MIXED
The public record is thin, but it is consistent on the core technical claim: 2 INFINITY LOGISTICS LLP is working on electromagnetic launchers for space payloads rather than terrestrial logistics software or freight services [Kerala Startup Mission, September 2025] [LinkedIn, October 2026]. Kerala Startup Mission describes the proposition as reducing the cost and environmental impact of launching payloads into space, while a LinkedIn profile describing an internship at the company says the work involved "delivering cargo in space with electromagnetic launchers" [PUBLIC] [Kerala Startup Mission, September 2025] [PUBLIC] [LinkedIn, October 2026]. Those are company-adjacent sources rather than independent technical validation, so they establish the stated product direction, not a demonstrated operating system, launcher build, or flight milestone.
The underlying physics is not speculative, but company-specific execution remains unproven in public. Historical technical literature cited here indicates electromagnetic launch concepts have been studied for payload delivery to low Earth orbit, with reported payload bands of 100 to 1,000 kg and exit velocities in the 4 to 6 km/s range under certain system designs [NASA Technical Reports Server (NTRS), 1985] [UNT Digital Library]. A separate NASA technical report discusses space mission applications for electromagnetic launchers and supports the broader category's technical plausibility [NASA Technical Reports Server (NTRS), 1989]. What is missing from the public evidence is the part investors usually need most: no verified prototype specifications, test results, subsystem architecture, launch cadence, customer payload requirements, or regulatory pathway have been surfaced in the cited materials.
That leaves the technology assessment in an early, concept-stage posture. The available sources support a narrow reading, namely that the company is positioning itself around electromagnetic launch infrastructure for space cargo and small-to-midweight payload classes, but they do not support stronger claims about readiness, differentiation, or commercialization timing [Kerala Startup Mission, September 2025] [LinkedIn, October 2026] [UNT Digital Library]. No tech stack inference is warranted from the captured job-posting set because those postings are unrelated to this company and cannot be used as evidence here.
Company-stated, unverified -- Product direction is supported primarily by company-adjacent directory and LinkedIn sources, while the technical feasibility discussion relies on independent category literature rather than company-verified performance data.
Where the Demand Sits
PUBLIC
The market matters now because any credible path to cheaper orbital delivery sits at the intersection of two active pressures: launch demand is broadening beyond national space agencies, while cost and emissions scrutiny are tightening across transport and industrial systems, making alternative launch architectures newly relevant even when they remain early [Kerala Startup Mission, September 2025] [NASA Technical Reports Server (NTRS), 1985] [UNT Digital Library, retrieved 2026].
Public evidence does not support a conventional TAM, SAM, and SOM build for this company or even for its precise wedge, electromagnetic launchers for space cargo. No named third-party market report was captured in the source set, and the record does not establish a defined initial customer segment, booked demand, or target launch class for 2 INFINITY LOGISTICS LLP [Kerala Startup Mission, September 2025] [Tofler, May 2025]. The more defensible read is narrower: this is a bet on an adjacent portion of the launch market where payload operators value lower cost per kilogram and where non-chemical systems could matter if the physics can be translated into a commercial service. The technical literature cited here frames that adjacent opportunity in payload terms rather than revenue terms, with studies describing electromagnetic launch concepts for 100 to 1,000 kg payloads to low Earth orbit and, in earlier NASA work, payloads of 800 kg or more [UNT Digital Library, retrieved 2026] [NASA Technical Reports Server (NTRS), 1985].
The demand drivers are easier to see than the addressable-market math. Kerala Startup Mission's profile states that the company's proposition is to reduce both launch cost and environmental impact, and those are not arbitrary claims for this category [Kerala Startup Mission, September 2025]. The technical sources explain why founders keep returning to electromagnetic launch concepts: reported exit velocities of 4 to 6 km/s imply a route toward materially reducing the propulsion burden for at least part of an orbital mission, with the economic case resting on reusable ground infrastructure and lower reliance on conventional propellants if the system works as designed [UNT Digital Library, retrieved 2026]. That does not establish near-term commercial viability, but it does explain the underlying market pull.
The closest adjacent markets are small-satellite launch, in-space cargo delivery, and mission architectures that can tolerate non-traditional launch profiles. The public footprint points to "delivering cargo in space with electromagnetic launchers," which suggests that the company may be thinking beyond a generic launch-service label and closer to a logistics layer for payload movement, though that remains a company-linked description rather than independent reporting [LinkedIn, October 2026]. Substitute solutions are straightforward: conventional rockets remain the incumbent, and any customer evaluating an electromagnetic system would compare against existing rideshare and dedicated-launch options on price, reliability, payload constraints, and schedule. The relevant regulatory and macro forces are also clear in outline, even if not yet company-specific: orbital systems face safety, export-control, and launch-approval scrutiny, while capital intensity remains high for any infrastructure-heavy space program [Ministry Of Corporate Affairs, retrieved 2026] [NASA Technical Reports Server (NTRS), 1989].
| Cited sizing or technical proxy | Figure | Context |
|---|---|---|
| Payload range | 100 to 1,000 kg | Electromagnetic coilgun launcher concept for space applications [UNT Digital Library, retrieved 2026] |
| Payload threshold | 800 kg or more | NASA mission-applications analysis for electromagnetic launchers [NASA Technical Reports Server (NTRS), 1985] |
| Exit velocity | 4 to 6 km/s | Technical literature describing launcher performance sufficient for LEO-oriented concepts [UNT Digital Library, retrieved 2026] |
The table does not size a market in dollars, but it does anchor the practical envelope the public research actually supports. For investors, that means the market case still depends less on headline space-economy growth and more on whether this architecture can eventually serve a specific payload class with a cost or emissions advantage that survives regulation and reliability requirements.
Lightly corroborated -- Built primarily from Kerala Startup Mission, NASA technical literature, and UNT technical literature; the market framing is partially corroborated, but company-specific demand and market-size evidence are limited.
Competitive Landscape
MIXED The company is positioned less against conventional launch providers than against the full stack of ways a payload can reach orbit, from rockets to high-altitude air launch concepts to other electromagnetic launch research programs, and that matters because the burden of proof sits on physics, manufacturability, and customer qualification rather than on branding alone [Kerala Startup Mission, September 2025] [NASA Technical Reports Server (NTRS), 1985] [UNT Digital Library, retrieved 2026].
The public record does not name direct commercial competitors, so the clearest way to map competition is by segment. In the incumbent lane sit rocket launch providers, which already offer flight heritage, customer procurement pathways, and regulatory muscle, even if they do not match the environmental or cost proposition implied by electromagnetic launch concepts [Kerala Startup Mission, September 2025]. In the challenger lane sit electromagnetic launch efforts described in research literature, where the technical case has been explored for decades, including analyses suggesting payload classes of 100 to 1,000 kg and exit velocities in the 4 to 6 km/s range under certain system designs [NASA Technical Reports Server (NTRS), 1985] [NASA Technical Reports Server (NTRS), 1989] [UNT Digital Library, retrieved 2026]. Adjacent substitutes include any mission architecture that reduces launch cost without using ground-based electromagnetic acceleration, because the buyer ultimately pays for orbit access, not for a specific propulsion philosophy.
Where the company appears to have an edge today is local institutional access rather than demonstrated commercial advantage. Kerala Startup Mission lists 2 INFINITY LOGISTICS LLP as a certified startup and frames the proposition around lower-cost, lower-impact payload launch, which gives the company a public foothold inside a state startup ecosystem even though it does not establish technical validation or customer demand [Kerala Startup Mission, September 2025]. The founding footprint is also concentrated: public filings identify Thazhamtharayil Selvarajan Sandeep and Swathi Thazhantharayil Selvarajan as designated partners, while LinkedIn evidence associates Sandeep with Carnegie Mellon University and identifies him as founder and CEO, a signal of technical ambition but not yet a durable moat on its own [Tofler, May 2025] [LinkedIn, retrieved 2026]. That edge is perishable unless it converts into proprietary test data, protected designs, or funded infrastructure, none of which is evidenced in the public record [Kerala Startup Mission, September 2025] [Tofler, May 2025].
The company is most exposed where established launch channels already own trust and where electromagnetic systems face constraints that research papers can discuss more easily than startups can finance. NASA and academic materials support the broad proposition that electromagnetic launchers can reach payload-relevant masses and velocities, but those same materials also imply a high bar in systems engineering, energy delivery, payload survivability, and downstream orbital insertion requirements [NASA Technical Reports Server (NTRS), 1985] [NASA Technical Reports Server (NTRS), 1989] [UNT Digital Library, retrieved 2026]. With no confirmed funding round, no named customers, and only ₹0.10 lakh in LLP capital contribution on Tofler, 2 INFINITY LOGISTICS LLP does not yet show the capital base that a hardware-heavy launch alternative would typically need to outrun conventional providers or better-funded research programs [Tofler, May 2025]. The practical competitor, then, is not a named startup so much as the incumbent rocket ecosystem's readiness advantage.
The most plausible 18-month scenario is a sorting between concepts that can produce third-party-credible test evidence and those that remain at the idea stage. If technical demonstrations, grants, or university-linked validation emerge, 2 INFINITY LOGISTICS LLP could become a local winner in the narrow sense of attracting early research attention around electromagnetic launch infrastructure in India, with Kerala Startup Mission remaining the clearest named institutional backer in public view [Kerala Startup Mission, September 2025]. If that evidence does not appear, the likely loser is the electromagnetic-launch proposition at the company level rather than the scientific idea itself, because incumbent rocket providers would continue to win customer budgets by default through existing launch availability and procurement familiarity. On present evidence, competition is decided less by concept originality than by who can turn a promising physics case into a financed, testable program.
Lightly corroborated -- Based primarily on Kerala Startup Mission, Tofler, LinkedIn, and historical NASA and academic materials; no named commercial competitors or independently reported market-share evidence were identified in public sources.
Opportunity
PUBLIC
If 2 INFINITY LOGISTICS LLP can turn electromagnetic launch from a research concept into an operating launch system, the prize is not a marginal improvement to logistics but a new low-cost access layer for certain classes of space payloads [Kerala Startup Mission, September 2025] [NASA Technical Reports Server (NTRS), 1985] [UNT Digital Library].
The headline opportunity is straightforward: become a specialist launch infrastructure company for payloads that can tolerate high-acceleration profiles, where lower cost and lower propellant use matter more than matching the flexibility of conventional rockets. That outcome is still early and conditional, but it is not purely aspirational on the physics. Public descriptions tie the company specifically to electromagnetic launchers for cargo to space [Kerala Startup Mission, September 2025] [LinkedIn, October 2026], and older technical literature shows the underlying approach has long been studied for orbital and near-orbital applications, including payload bands from roughly 100 kg to 1,000 kg and exit velocities in the 4 to 6 km/s range [NASA Technical Reports Server (NTRS), 1985] [UNT Digital Library]. The reachability here comes from technical precedent, not from evidence of commercial traction.
The upside paths are easier to see than the execution proof. Publicly, the company is a 2023-incorporated Kerala startup with a limited corporate and operating footprint so far [Tofler, May 2025] [Kerala Startup Mission, September 2025]. That means the opportunity case rests on whether a small team can move from concept framing into demonstrable hardware, then into a regulated launch product, then into repeat demand from payload operators. The category can support that kind of leap if the cost and environmental claims hold in practice, because launch economics are still constrained by expensive propulsion systems and low cadence for many use cases [Kerala Startup Mission, September 2025] [NASA Technical Reports Server (NTRS), 1989].
| Scenario | What happens | Catalyst | Why it's plausible |
|---|---|---|---|
| Orbital cargo wedge | The company focuses on cargo or payload classes suited to electromagnetic launch and becomes a specialist provider for low Earth orbit insertion support | A successful hardware demonstration showing target exit velocities or payload handling aligned with published electromagnetic-launch benchmarks | Electromagnetic launcher literature supports space applications at 4 to 6 km/s exit velocity and payload classes from 100 to 1,000 kg, which gives a technical envelope for an initial niche [UNT Digital Library] [NASA Technical Reports Server (NTRS), 1985] |
| Public-sector R&D partner | The company becomes a research and prototyping partner for state or institutional space programs before becoming a full commercial launcher | Deeper programmatic support through startup or public innovation channels in Kerala and India | The company is already listed as a certified startup by Kerala Startup Mission, which is the clearest public institutional connection today [Kerala Startup Mission, September 2025] |
| Green launch alternative | The company wins attention as a lower-environmental-impact launch option for specific payload categories and attracts payload operators that value lower propellant intensity | A pilot customer, research partnership, or validation milestone tied to environmental performance | The company's public proposition is explicitly framed around reducing both launch cost and environmental impact, and that framing aligns with longstanding interest in electromagnetic alternatives to conventional launch propulsion [Kerala Startup Mission, September 2025] [NASA Technical Reports Server (NTRS), 1989] |
What compounding would look like is a hardware learning curve rather than a software network effect. One validated launch subsystem can improve the next through better materials choices, power-delivery tuning, guidance integration, and payload qualification, while each institutional partner can shorten the path to the next one. There is no public evidence yet that this flywheel has started commercially, but the company has at least chosen a narrow enough technical thesis, electromagnetic launch for space cargo, that progress could compound if early demonstrations produce defensible know-how [LinkedIn, October 2026] [Kerala Startup Mission, September 2025].
The size of the win is best framed as infrastructure value capture, not near-term startup revenue. No public market-size figure is confirmed in the source set, and there is no named direct comparable in the provided evidence, so any valuation framing has to stay conditional. If the company were to prove a repeatable launch system for a meaningful subset of payloads and become a recognized launch infrastructure supplier, the outcome could support venture-scale value creation because launch providers sit close to mission-critical spend in the space stack (scenario, not a forecast) [NASA Technical Reports Server (NTRS), 1985] [NASA Technical Reports Server (NTRS), 1989]. At this stage, the upside case is real mainly because the problem is large and the technical proposition addresses a hard cost bottleneck, not because the company has yet shown public evidence of product-market fit.
Company-stated, unverified -- This section relies on company-adjacent directory and LinkedIn descriptions for the startup's current activity, with technical plausibility supported by NASA and UNT research rather than verified operating results.
Sources
Public sources
[Kerala Startup Mission, September 2025] 2 INFINITY LOGISTICS LLP | Kernel Platform - Kerala Startup Mission | https://startups.startupmission.in/startups/0BwQK
[Tofler, May 2025] 2 INFINITY LOGISTICS LLP | Tofler | Company Research Platform | Organizing business information from around India | https://www.tofler.in/2-infinity-logistics-llp/company/ACD-0275
[LinkedIn, October 2026] LinkedIn profile, Shubhamoy Halder | https://www.linkedin.com/in/shubhamoyhalder
[UNT Digital Library, retrieved 2026] Electromagnetic coilgun launcher for space applications | https://digital.library.unt.edu/ark:/67531/metadc626274/
[NASA Technical Reports Server (NTRS), 1985] Preliminary analysis of space mission applications for electromagnetic launchers - NASA Technical Reports Server (NTRS) | https://ntrs.nasa.gov/citations/19850003763
[LinkedIn, retrieved 2026] Sandy ( Sandeep ) T Shelvan - Wharton | Carnegie Mellon | https://www.linkedin.com/in/sandeep-t-shelvan/
[Ministry Of Corporate Affairs, retrieved 2026] Ministry Of Corporate Affairs - Disclosure,Audit and Filing Requirements | https://www.mca.gov.in/MinistryV2/disclosureauditandfilingrequirements.html
[NASA Technical Reports Server (NTRS), 1989] Electromagnetic launchers for space applications - NASA Technical Reports Server (NTRS) | https://ntrs.nasa.gov/citations/19890044698
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