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The trajectory, strike per rupee

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Apollyon Dynamics · Strategy

Apollyon sells machines, but the strategy underneath them is bigger: bring down what India pays for long-range strike, and build the sovereign industrial and software foundation to keep driving down the cost of effect across an expanding, diversified portfolio of autonomous platforms. Today's jet-powered effectors and cruise missiles are the starting platforms; this page is the arithmetic behind the trajectory.

01 · Objective

What we optimise

For fifty years, defence primes were paid to maximise capability per airframe. Each generation added stealth, sensors and integration work; unit costs rose; the quantities bought fell. Recent wars have settled the argument: what decides who can keep fighting is how much can be produced, how fast it can be replaced, and what each round costs to lose.

Apollyon measures something else: strike effect per rupee spent. While the immediate production focus is a family of jet-powered one-way effectors and cruise missiles built on one autopilot baseline and one engineering method, the broader mandate is to leverage this common autonomy, guidance, and manufacturing architecture to rapidly spawn and diversify into new autonomous platforms and domains—relentlessly driving down the cost of delivered effect with every generation.

Two definitions make that measurable, and the rest of this page follows from them.

02 · Definition

The unit we count in

Comparing weapons by unit price or range alone obscures delivered effect. A commander buys warhead mass delivered across distance. Combining payload and range yields total delivered strike work:

Governing Equations
Strike Envelope [kg·km] = Payload (kg) × Range (km)
Cost per Effect [₹/kg·km] = Unit Cost (₹) ÷ Strike Envelope
• Nightshade Mk II: 15 kg × 300 km = 4,500 kg·km  →  ₹1.5 Cr ÷ 4,500 ≈ ₹3,333 / kg·km
• Hemlock: 450 kg × 1,500 km = 675,000 kg·km  →  ₹4 Cr ÷ 675k ≈ ₹59 / kg·km

Normalizes tactical loitering munitions and heavy cruise missiles onto a single capital-efficiency axis.

Two rules qualify this metric: the airframe must clear electronic-warfare and autonomous terminal accuracy gates, and survivability assumes subsonic terrain masking and route planning.

03 · Measurement

The metric, measured against the field

Today's Apollyon systems sit at roughly ₹3,300–3,500 per kg·km. Hemlock is specified toward ₹55–60 — roughly an order of magnitude below the comparators, and lower than anything currently fielded at its range.

Fig. 01log–log · lower is better
₹10₹100₹1,000₹10,0001503005001,0001,5002,000LOWER IS BETTER ↓· UNIT COST ÷ (PAYLOAD × RANGE)OPERATIONAL RANGE, KM (LOG SCALE)COST PER KG·KM (INR)Berkut-BM₹4,500Barracuda-250₹3,200Barracuda-500₹500Tomahawk₹480Nightshade Mk II₹3,333 / kg·kmHemlock₹59 / kg·kmabout 8× below TomahawkIN SERVICEAPOLLYONUSD 1 = INR 95 · Comparator prices from public sources · Berkut-BM unit cost estimated
Fig. 01 Unit cost ÷ (payload × range). In-service comparators in grey, the Apollyon family in red. The staircase descends because each generation inherits the guidance core and pays only its delta.

The Ukrainian benchmark we are chasing

Ukraine's FP-5 Flamingo is the honest benchmark for effect per rupee: a 1,150 kg penetrator, a claimed 3,000 km, estimated at $0.5–1M per round on salvaged engines. On this metric it is extraordinary — roughly ₹20/kg·km on the round, or about ₹60 per kg·km on the arriving round at its observed ~1-in-3 hit rate.

That distinction is the strategy. Flamingo buys effect with salvo mass and accepts the misses because its economics permit it; it is also capped by a finite stock of surplus engines, which is why Fire Point is building its own turbojet and why output sits near three rounds a day against a target of seven. Apollyon's route to the same economics is different: keep arrival probability high, remove the subsystems that make cruise missiles expensive, and let the engineering base fall in cost with every generation.

Two routes to affordable effect planning figures
SystemPayloadRangeEnvelopeCost / round₹ / kg·km (round)Arrival-adjusted
FP-5 Flamingo observed1,150 kg3,000 km3.45M kg·km$0.5–1M est.≈ ₹20≈ ₹60 at ~1-in-3
Hemlock450 kg1,500 km675K kg·km≈ $0.45M est≈ ₹59≈ ₹59–70
Tomahawk Block V~450 kg~1,600 km0.72M kg·km~$1.9M≈ ₹480≈ ₹480
Barracuda-500M45 kg926 km41.7K kg·km~$216k≈ ₹500≈ ₹500
Berkut-BM10 kg150–180 km~1.6K kg·kmest.≈ ₹4,500≈ ₹4,500

Flamingo, Tomahawk and Barracuda figures from public reporting and manufacturer disclosures; Apollyon costs are internal planning figures, not quotes. Arrival-adjusted cost divides by observed or specified hit probability and is indicative only.

04 · Family

The family, and what each generation costs to run

Generation economics planning figures
SystemPayloadRangeEnvelopeTop speedRound cost (est.)₹ / kg·kmStatus
Nightshade Mk I—20 kmPoC700 km/h——Flown 2026
Nightshade Mk II
Loitering Munition (turbojet)
15 kg300 km4,500 kg·km700 km/h≈ ₹1.5 Cr≈ ₹3,333Prototype Q1 2027
Hemlock450–500 kg1,000–1,500 km675K kg·km~900 km/h≈ $450k≈ ₹59Concept · production 2030–31
Fig. 02envelope per generation
STRIKE ENVELOPE — PAYLOAD × RANGE (KG·KM, LOG SCALE)101001K10K100K1M20NIGHTSHADE MK IFLOWN 2026Airframe andPerformance test20 km range · No warhead700 km/h flight test4,500NIGHTSHADE MK II2027Loitering Munition+ Target Drones15 kg payload · 300 km700 km/h terminal dive675,000HEMLOCK2030–31Long-RangeCruise Missile450–500 kg · 1,000–1,500 km860–980 km/hMk I carries no payload and flies a minimal guidance fit; every system above it inherits the same engineering base.
Fig. 02 The envelope staircase. Mk I flight-tests the airframe and carries no payload; from Mk II onward each system inherits the method, the supplier base and the qualification evidence, which is why the curve rises per unit of development money spent rather than only per round.

Each generation inherits what the last one proved and pays only for what is new:

What each generation pays for
GenerationInheritsPays only the delta
Nightshade Mk I— · airframe testAirframe, first engine integration, GNSS-only navigation
Nightshade Mk IINavigation, estimation, control, softwareAirframe scale, launch system, seeker integration
HemlockMethod, models and qualification evidenceHeavy airframe, Manik 450 turbofan, 450–500 kg warhead, its own guidance implementation

Programme roadmap

Four programmes on one core. Red marks the year in progress, filled bars are production events already committed, and dashed bars are design work still to be earned.

Programme roadmap2026 · 2030
Platform20262027202820292030
NightshadeTarget Drone (Economical / Premium) / Loitering Munition Mk II
Target-drone prototype Mk II LM prototype · production starts Mass production
AhutiCounter-UAS interceptor
Flight trials · 498 km/h record Mass production
PiranhaUnmanned surface vessel
Hull build · sea trials from late 2026 Sea trials · qualification Serial production
HemlockLong-range cruise missile
Concept Design & bench Prototype 2029 Production 2030–31
Year in progress Production event Planned design work
Roadmap Nightshade flies its target-drone prototypes in Q4 2026 and the Mk II loitering-munition prototype in Q1 2027, with mass production in 2028; Ahuti moves to Make-II volume and private sales in 2027; Piranha builds its hull and hardware in 2026, starts sea trials at the end of 2026 and moves to serial lines from 2028; Hemlock is in concept in 2026 and runs design and bench qualification through 2027–28, with the prototype in 2029 and production from 2030–31.
05 · Decisions

The decisions that set the cost

Three architectural principles dictate our development trajectory. Each represents an intentional departure from traditional defence contractor practices:

  1. Preserve the common baseline: The Nightshade configurations share one autopilot baseline and one configuration lineage: guidance modes, control packages, envelope limits, safety logic and telemetry protocols. Apollyon refines the configuration continuously and folds validated changes back across the line; later programmes such as Hemlock inherit the method and the qualification evidence rather than starting from a blank sheet.
  2. Compress recurring research and development expenses: The initial flight demonstrator absorbed the capital cost of core development. Subsequent platforms inherit this baseline, directing engineering capital toward airframe tooling, engine integration, and warhead packaging. Capital expenditure yields expanding strike envelopes with each generation, documented through accumulated qualification records.
  3. Advance operational doctrine alongside hardware: Nightshade Mk II delivers precision tactical strikes. Hemlock operates as a long-range strike weapon—designed to neutralise hardened infrastructure while mixed salvos exhaust defensive interceptor stockpiles. The same engineering base serves both operational roles without starting a bespoke development programme.

Unit costs are controlled by eliminating expensive legacy subsystems. We avoid proprietary military-grade inertial gyro blocks, custom mechanical gyroscopes, and decade-long component qualifications that elevate legacy cruise missile prices. Instead, we combine progressive metal stamping, commercial automotive servos, out-of-autoclave composites, and hardened edge silicon.

Engineering boundary: capability preservation

Cost control does not mean stripping tactical capability. Every strike effector retains four-layer navigation, passive terminal thermal imaging via Tonbo, independent abort channels, and encrypted telemetry. We remove legacy aerospace over-engineering, not mission performance.

06 · Procurement

What the requirement sheet has to ask for

India's heavy strike weapons are already in serial production — BrahMos and Pralay at an officially stated 100–200 rounds a year — but at ₹25–35 crore a round they are priced for the highest-value targets. A sovereign attritable layer requires procurement frameworks that incentivize high-tempo manufacturing. Monthly production output, part counts, and domestic supplier depth must serve as formal evaluation criteria.

Peacetime procurement metrics versus wartime production criteria
Peacetime boutique procurementWartime replenishment procurement
Maximum range — kmUnit cost at volume production — ₹ / round
Cruise speed — MachAssembly labour — hours / round
Circular error probable — mUnique custom part count — count
Warhead mass and chemistry — kgQualified domestic suppliers per critical part — ≥ 2
Launch platform interface compatibility — interfaceSustained monthly manufacturing capacity — rounds / month
Environmental qualification — MIL-STDReplenishment lead time — weeks; domestic content by value — %; depot storage life — years

Apollyon structures Make-II and iDEX defence proposals around volume replenishment metrics. High-intensity modern combat depletes peacetime magazines in weeks. Deterrence requires manufacturing capacity capable of replacing tactical losses in continuous production runs.

07 · Arithmetic

Why the mixture wins

Attritable effectors do not eliminate heavy cruise missiles; they optimize their delivery. Standoff strike doctrine requires mixed salvo architectures fired against finite defensive interceptor magazines. In our baseline scenario, an attacker budget is split between attritable effectors and heavy cruise missiles against a defended sector of 120 soft targets and 15 hardened installations. The defending battery maintains 400 interceptor missiles firing two rounds per track with a 75% single-shot kill probability.

Fig. 03salvo model · all constants exposed
0%25%50%75%100%0%25%50%75%100%MAGAZINE RUNS DRYBEST SPLIT 46%69% of objectivesOBJECTIVES METSHARE OF BUDGET SPENT ON ATTRITABLE ROUNDSATTRITABLE FIRED FIRSTEXQUISITE FIRED FIRSTAll-exquisite leaves most targets untouched; all-attritable clears the soft set and nothing hardened.The mixture beats both corners, and the firing order is worth as much as the mixture.
Fig. 03 Objectives met against the share of budget spent on attritable rounds. All-exquisite leaves most targets untouched; all-attritable clears the soft set and nothing hardened. The mixture beats both corners, and the firing order — attritable first — is worth as much as the mixture.

Three results emerge consistently across salvo simulations. Salvos of only the most expensive weapons run out too early: a limited missile budget cannot service 135 aim points, meaning 135 separate targets to be hit, so the defending batteries get time to engage all inbound tracks. Salvos of only cheap, disposable weapons can only hit unprotected targets: hardened concrete revetments survive light warhead impacts. Mixed salvos work best: inexpensive effectors fired first overwhelm the radars' ability to track incoming weapons and use up the defending side's surface-to-air missiles, so follow-on cruise missiles can strike hardened installations through the gaps this leaves in the air defence.

Our product architecture reflects this operational firing order: Nightshade loitering effectors strip radar coverage and deplete magazines, while Hemlock heavy effectors neutralize hardened command points. Maintaining high terminal arrival probabilities remains essential—an effector with a 70% arrival rate achieves superior campaign economy compared to platforms landing one in three.

08 · Diligence

What has to be true

Strategic roadmaps require concrete empirical validation. The following operational milestones define program progress across our product lines:

Conditions, status, and what closes each one
ConditionStatusVerification milestone
Flight-validated core on jet airframesMk I demonstrated GNSS flight; Mk II adds the full navigation and seeker fitNightshade Mk II loitering-munition prototype flight campaign, Q1 2027
Unit cost curve validation at rateInternal engineering planning figuresSigned supply chain production contracts against initial rate orders
Propulsion supply depthThree qualified engine sources for Nightshade; Hemlock requires Manik 450 kgf turbofan rateStanding Manik rate agreement with BrahMos Aerospace (BATL)
Seeker manufacturing volumeTonbo Imaging strategic partnership finalizedLong-term volume procurement agreement supporting Mk II serial production
Integrated cUAS command softwareAhuti effectors deployable with external integratorsDKS consortium integration and open battery C2 interoperability
Battery cell supply chain independenceActive qualification gap on interceptor lineDual-sourced Indian and allied high-discharge lithium cells—see supply chain
Volume procurement authorizationActive Make-II and iDEX engagementFormal tender releases specifying monthly delivery throughput and rate pricing

Read in conjunction with the competitive field and the supply chain, these criteria provide clear, testable verification milestones for technical diligence.

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