<2025> Secondary Battery Technology Development Status and Market Outlook for UAM/UAV (Drones)
UAM
(Urban Air Mobility) and UAVs (drones) are no longer viewed merely as “new
technologies,” but are increasingly recognized as core mobility platforms that
will transform urban structures and industrial ecosystems over the next 10–20
years. Both technologies are based on electric propulsion, autonomous flight,
and digital traffic management, with high-energy and high-safety battery
technologies in particular determining the success or failure of
commercialization.
From a
social change perspective, the introduction of UAM is expected to bring
fundamental changes to urban transportation systems. As eVTOL aircraft
operating at altitudes of 300–600 m above urban areas connect airport–city and
city–city routes of 20–50 km within 10–20 minutes, a portion of existing ground
transportation demand will shift to the air, forming a new three-dimensional
transportation network. This goes beyond simply adding a new mode of transport
and may affect the overall urban spatial structure, including improved airport
accessibility, enhanced efficiency of intercity travel, and the reshaping of
commercial and real estate values in specific areas.
UAM
technology is advancing based on electric vertical take-off and landing (eVTOL)
platforms. Many global companies have entered the prototype flight testing and
certification stages, with competitors including Joby and Archer in the United
States, Volocopter in Germany, EHang and XPeng AeroHT in China, and SkyDrive in
Japan.
In China,
EHang has reached the stage of commercial operations by sequentially securing
the world’s first type certification, airworthiness certification, and
production certification for a dual-purpose unmanned/manned eVTOL (EH216-S).
Meanwhile, XPeng AeroHT is expanding urban flight demonstrations through the
development of the X2 and flying car models (X3 and X4 prototypes).
UAVs
(drones) are already approaching a mature market. Chinese manufacturers led by
DJI account for more than 70% of the global market, and a wide range of drone
solutions have been commercialized across agriculture, public safety,
logistics, and industrial inspection applications. In the high-end industrial
drone segment, advanced technologies such as automated take-off and landing
pads, LTE- and 5G-based remote operations, swarm flight, and AI-based image
analysis are rapidly evolving.
In the aircraft platform segment, the global UAM market size was at the level of several billion dollars in 2023, but major institutions project that it will grow to approximately USD 20–30 billion by 2030 and exceed USD 40 billion by 2035. This represents a high CAGR of around 20–30% and symbolizes a transition phase in which UAM enters the realm of “next-generation air transportation.”
The global
commercial drone market is estimated at around USD 30 billion in 2024 and is
expected to grow to approximately USD 50–55 billion by 2030. In particular, the
data analytics and drone-as-a-service (DaaS) market is expanding more rapidly
than hardware, and as demand for industrial efficiency and automation
continues, the overall market size is expected to steadily increase.
In the
battery market segment, the
UAM/eVTOL-dedicated battery market is estimated to be at the level of several
hundred million to approximately USD 0.5 billion as of 2024. However, as UAM
commercialization accelerates in the early 2030s, the market is projected to
expand to around USD 4.5 billion. Some market research firms also forecast that
the eVTOL battery market will grow at a CAGR of more than 20–25% during the
2025–2033 period.
The UAV
(drone) battery market is projected to grow from approximately USD 1–9 billion
during 2023–2025 to USD 2–50 billion by 2030–2035. While estimates vary
depending on definitions, a generally high annual growth rate in the range of
8–20% is expected.
Meanwhile,
from a battery development perspective, UAM and UAV applications require
battery performance standards far more stringent than those for electric
vehicles. This is because both sectors are fully subject to aviation safety
regulations while relying almost entirely on electric propulsion systems. In
particular, eVTOL aircraft must simultaneously meet requirements for extremely
high peak power during vertical take-off and landing, lightweight design, high
energy density (exceeding 300–400 Wh/kg), robust thermal safety, short charging
times, and compliance with aviation safety standards. UAVs, depending on
mission profiles, require a balanced combination of high power, light weight,
low-temperature performance, high C-rate capability, and operational stability.
At
present, most UAM prototypes use high-energy cells based on high-nickel NCM and
NCA chemistries, with some models adopting silicon anode–based cells. UAVs
typically employ lithium-polymer (Li-Po) batteries or high-power 18650 and
21700 cylindrical cells that offer excellent charge–discharge performance.
Most eVTOL
aircraft use battery packs based on high-nickel NCM and NCA cells, targeting a
pack-level energy density of approximately 250–300 Wh/kg. Because this level
demands higher safety margins and high-power designs compared with current
electric vehicles, development extends beyond the cells themselves to include
pack structural design, thermal management (cooling and insulation),
multi-layer BMS architectures, and fire prevention and isolation between cell
modules, all of which are being developed as an integrated technology package.
UAVs
(drones) span a wide spectrum depending on their applications. Consumer and
small commercial drones primarily use high-discharge lithium-polymer (LiPo)
batteries and 18650/21700 cylindrical cells, while industrial and military
drones often combine high-energy and high-power cells with specialized pack
designs. For medium- to long-range missions where long endurance is critical,
some platforms adopt fuel cell systems, such as Doosan Mobility Innovation
(DMI)’s hydrogen fuel cell drones. In addition, development is underway in
parallel on “electric + fuel cell” hybrid energy systems, including
battery–fuel cell hybrid configurations.
Meanwhile,
next-generation battery development is one of the most active areas in UAM and
UAV battery research. Various technology reviews and market studies identify
UAM and eVTOL platforms as leading candidates for early commercialization of
lithium-metal, lithium–sulfur, all-solid-state, and bipolar batteries.
Lithium-metal and lithium–sulfur systems, which theoretically offer energy
densities exceeding 400–500 Wh/kg, are regarded as promising options for
directly alleviating current limitations on eVTOL flight range and payload
capacity. However, challenges related to cycle life, dendrite formation, and
cell stability remain unresolved. All-solid-state batteries, meanwhile, are
attracting particular attention in aviation applications because their non-flammable
electrolytes can significantly reduce the risk of thermal runaway, and multiple
automakers and battery manufacturers are pursuing development with pilot
deployment targeted for the late 2020s.
In
summary, battery development for UAM and UAV applications is currently at a
stage where the aviation optimization of high-performance lithium-ion
batteries—balancing safety, power output, and energy density—and early
commercialization efforts for next-generation batteries such as lithium-metal,
all-solid-state, and lithium–sulfur systems are progressing in parallel. The
competition is no longer limited to producing high-quality cells alone; rather,
it is intensifying around integrated solutions that encompass pack design
tailored to aviation regulations and mission profiles, along with thermal
management, BMS, and operational software. This domain is likely to become one
of the strategic battlegrounds in the battery industry over the next decade.
This
report aims to present a clear and accessible overview of the current market
status and development trends of UAM and UAV (drone) technologies, which have
recently emerged as hot topics, and to systematically summarize the battery
requirements and the status of next-generation battery development applied in
these fields to facilitate understanding.
This
report has the following key features and strengths.
①
Detailed coverage of UAM (eVTOL) aircraft and core system
technologies
②
Comprehensive overview of battery requirements for eVTOL/UAM
applications (performance, power output, lifetime, and safety)
③
Inclusion of results from demonstration studies on lithium-ion
batteries for eVTOL applications (load conditions, cycling behavior,
degradation, and post-mortem analysis)
④
In-depth coverage of the development status of next-generation
batteries (Li-metal, all-solid-state, semi-solid-state, Li–S, high-nickel, and
bipolar batteries)
⑤
Detailed analysis of companies and market trends related to
UAM and UAV (drone) industries
INDEX
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|
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1.
Global eVTOL/UAM Market And Industry Trends
|
|
1-1 eVTOL R&D Boom And
Market Consolidation Outlook
|
11
|
1-2 Background Of The
Emergence Of eVTOL
|
12
|
1-3 eVTOL Technology
Architecture, Safety, And Industry Status
|
13
|
1-4 eVTOL Industry Trends
|
14
|
1-4-1
Characteristics By Application / Business Model / Region
|
14
|
1-4-2
Technology, Regulation, And Player Trends
|
15
|
1-4-3
Status Of Major Global Companies
|
16
|
1-5 eVTOL Market
|
17
|
1-5-1
Types By Application Scenario
|
17
|
1-5-2
Market Size And Growth Rate Outlook
|
18
|
1-5-3
Analysis Of Core Subsystems And Cost Structure
|
19
|
1-5-4
Major Investment Flows And Trends
|
20
|
|
|
2. Low-Altitude Economy And UAM National Policies And Global Comparison
| |
2-1 Status Of The Low-Altitude
Economy
|
21
|
2-1-1
United States And Europe
|
21
|
2-1-2
Korea And Japan
|
22
|
2-1-3
China
|
23
|
2-1-4
Chinese Companies
|
24
|
2-2 China’s Low-Altitude Economy
|
25
|
2-2-1
Three Priority Principles For Development
|
25
|
2-2-2
Status Of Key Industries And Capital Market Performance
|
26
|
2-2-3
Recent Major Events (May–June 2025)
|
27
|
2-3 China’s UAM / Drone / Aviation Industry
|
28
|
2-3-1
eVTOL
|
28
|
2-3-2
Drone
|
29
|
2-3-3
General Aviation And UAV
|
30
|
2-4 Status Of National UAM /
UAV / Drone Programs By Country
|
31
|
2-5 Korea’s UAM Industry: Industry Status And Expansion Plans
|
32
|
2-5-1
Related Industry Status And Expansion Plans
|
32
|
2-5-2
K-UAM Implementation Status And Roadmap
|
33
|
2-6 China’s UAM Industry: Related Industry Status And Expansion
Plans
|
34
|
2-7 Japan’s UAM Industry
|
35
|
2-7-1 Related Industry Status And Expansion Plans
|
35
|
2-7-2
Commercialization Of Aircraft Propulsion Systems By NEDO
|
36
|
2-8 U.S. UAM Industry: Related
Industry Status And Expansion Plans
|
37
|
2-9 Europe’s UAM Industry: Related Industry Status And Expansion
Plans
|
38
|
|
|
3. eVTOL Aircraft / Structure / Configuration Methods And
Classification
| |
3-1 Definition And
Classification By UAM Aircraft Type
|
40
|
3-2 eVTOL Classification
(Based On Vertical Flight Society)
|
41
|
3-3 eVTOL Aircraft
|
44
|
3-3-1
Product Specifications (1/2)
|
44
|
3-3-2
Product Specifications (2/2)
|
45
|
3-4 eVTOL Propulsion Methods
|
46
|
3-4-1 Comparison Of Three Representative Methods
|
46
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3-4-2
Comparison Of Four Representative Methods
|
47
|
3-5 eVTOL (Wingless
Multirotor)
|
48
|
3-5-1 Specifications And Battery Specs
|
48
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3-5-2
eHang 184 Specifications
|
49
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3-6 eVTOL (Lift + Cruise):
Specifications And Battery
|
50
|
3-7 eVTOL (Vectored Thrust):
Specifications And Battery
|
51
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3-8 eVTOL Power Comparison
|
52
|
3-9 eVTOL
|
53
|
3-9-1
Compound High-Speed Rotor Type
|
53
|
3-9-2
Rotor/Wing Conversion Type
|
54
|
3-9-3
Tilt-Rotor/Wing Type (1/2)
|
55
|
3-9-4
Tilt-Rotor/Wing Type (2/2)
|
56
|
3-10 Multi-Rotor eVTOL
Products And Specifications
|
57
|
3-11 Winged Compound eVTOL
Products And Specifications
|
58
|
3-12 Tilt-Rotor Wing eVTOL
Products And Specifications
|
59
|
3-13 Summary Of Advanced
Rotorcraft Development
|
60
|
|
|
4. eVTOL Core System Technologies (Electric Propulsion · Power Electronics · Sensing · Control)
| |
4-1 eVTOL Core System
Technologies
|
61
|
4-1-1
Electric Propulsion · Flight Control · Perception · Decision-Making · Safety
|
61
|
4-1-2
Motors And Power Electronics
|
62
|
4-1-3
Flight Control
|
63
|
4-1-4
Sensing & Perception
|
64
|
4-1-5
Safety & Reliability
|
65
|
4-6 Advances In DEP
(Distributed Electric Propulsion) Technology And Multi-Mode Transition Of
Tilt-Multirotors
|
66
|
4-7 eVTOL Autonomous Operation
Approaches (Overview: Piloted Path vs. Pilotless Path)
|
67
|
4-8 eVTOL Noise Standards And
Current Status
|
68
|
|
|
5. eVTOL Requirements And Design Trade-Offs Compared With Conventional
Aircraft
| |
5-1 eVTOL Requirements And
Design Trade-Offs Versus Conventional Aircraft (Helicopter vs. Fixed-Wing)
|
70
|
5-2 eVTOL Performance
Evaluation Methods – Reference
Missions And Comparison Framework
|
71
|
5-3 Definition Of Aircraft
Design Input Conditions And Short-Range Mission Profiles
|
72
|
5-4 Analysis Of The Impact Of
Changes In Aircraft Design Requirements On SoS Efficiency
|
73
|
5-5 Sensitivity Analysis
Results For Operational Procedures (Turnaround And Speed) And Demand Changes
|
74
|
5-6 Key Summary Of UAM
Aircraft Design And Operational Sensitivity Analysis
|
75
|
|
|
6. UAV Classification ·
Propulsion · Comparison / Renewable Energy–Based UAVs
| |
6-1 UAV Classification:
Geometric Structure, Size, And Mission Type
|
76
|
6-2 UAV Classification And
Specifications
|
77
|
6-3 UAV Propulsion Power
Sources
|
78
|
6-3-1
Comparison By Technology
|
78
|
6-3-2
Comparison Of Characteristics In Practical Applications
|
79
|
6-3-3
Battery
|
80
|
6-3-4
Fuel Cell
|
81
|
6-3-5
Solar Cell
|
82
|
6-3-6
Hybrid Power
|
83
|
6-3-7
Challenges – Current Status –
Perspectives
|
84
|
6-4 UAV Market Outlook And
Trends In The Number Of Research Publications
|
85
|
6-5 UAV Power Sources: Recent
Research On Energy Sources
|
86
|
|
|
7. Battery Requirements For eVTOL/UAM (Performance · Power Output · Lifetime · Safety)
| |
7-1 Battery Technologies For
eVTOL
|
87
|
7-2 eVTOL Battery Evolution
And Cost Analysis
|
88
|
7-3 eVTOL: Correlation Between
Disc Load And Hovering Efficiency
|
89
|
7-4 eVTOL Battery Requirements
|
90
|
7-4-1
Specific Power
|
90
|
7-4-2
Specific Energy
|
91
|
7-4-3
Fast Charging And Cycle Life
|
92
|
7-4-4
Safety And The Importance Of Fast Charging
|
93
|
7-4-5
Benchmark Battery (I): 215 Wh/kg Cell
|
94
|
7-4-6
Benchmark Battery (II): 271 Wh/kg Cell
|
95
|
7-5 Battery Requirements For
UAM And Development Status
|
96
|
|
|
8. Aircraft Electrification And UAM Battery Systems / Modules / Thermal
Management
| |
8-1 Shifts Toward Sustainable
Air Transportation
|
98
|
8-2 Outlook For Commercial
Aircraft Electrification And Electric Power Requirements
|
99
|
8-3 Electrification Of
Commercial Aircraft
|
100
|
8-4 Electrically Powered
Short-Range Aircraft
|
101
|
8-5 UAM Batteries: Research
Trends On Cell-to-Cell Non-Uniformity And Thermal Effects
|
102
|
8-6 LIB Module Design And
Experimental Setup For UAM
|
103
|
8-7 Experimental Results On
Internal Resistance And Heat Generation Characteristics Of UAM LIBs
|
104
|
8-8 Simulation & Thermal
Behavior: Thermal Behavior Analysis Results
|
105
|
8-9 Thermal Behavior Of UAM
Battery Modules And Design Implications
|
106
|
8-10 Impact Of Battery
Performance On UAM Operations
|
107
|
8-11 DOC (Direct Operating
Cost) Model For UAM Operational Economics And Combined Analysis Of Design
Factors
|
108
|
8-12 Key Battery Technology
Characteristics For UAM Operation And Current Trends
|
109
|
8-13 Validation Results Of The
DOC Model Through Analysis Of Existing Commercial UAMs
|
110
|
8-14 Analysis Of The Impact Of
C-Rate Characteristics On UAM Design Weight And Operating Modes
|
111
|
8-15 Impact Of Energy Density
Improvements (2035 Outlook) On UAM Economics And Range
|
112
|
|
|
9. Battery Modeling ·
Simulation · Electrode Structure Design
|
|
9-1 Battery P2D (Pseudo
Two-Dimensional) Modeling
|
113
|
9-2 Battery Microstructure
Surrogate Models
|
114
|
9-2-1 Overview Of Microstructure Surrogate Models
|
114
|
9-2-2 Application Of Microstructure Surrogate Models
|
115
|
9-3 Impact Of Electrode
Structure On Transport Properties And Constant-Current Discharge Performance,
And Derivation Of Optimal Structures
|
116
|
9-4 Comparison Of eVTOL
Operating Performance (Reference vs. Optimized) And Analysis Of ASSB State At
End Of Operation
|
117
|
9-5 Approaches To Improving
All-Solid-State Battery Performance: Materials And Microstructure
Optimization
|
118
|
9-6 Modeling Methodology – Integrated Simulation Framework For Flight Models
And Battery Models
|
119
|
9-7 Impact Of Changes In
Operating Conditions On Aircraft Performance And Battery Behavior
|
120
|
9-8 Battery Design Case Study
|
121
|
9-8-1
Analysis Of The Impact Of Electrode Geometric Structure Design (1)
|
121
|
9-8-2
Analysis Of The Impact Of Electrode Geometric Structure Design (2)
|
122
|
9-8-3
Analysis Of Electrode Material Properties / Pack Energy Capacity Variables
(1)
|
123
|
9-8-4
Analysis Of Electrode Material Properties / Pack Energy Capacity Variables
(2)
|
124
|
9-9 UBDM Modeling And
Degradation Mechanisms
|
125
|
9-10 Necessity And Research On
eVTOL Battery Performance Prediction
|
126
|
9-11 Cellfit Model And
Construction Of eVTOL-Specific Datasets
|
127
|
9-12 Performance Modeling
Results And Accuracy Of Cellfit
|
128
|
9-13 Development And
Comparison Of A Universal Battery Degradation Model (UBDM)
|
129
|
9-14 Performance Improvement
Using UBDM And Conclusions
|
130
|
|
|
10. Experimental Studies On LIBs For eVTOL Applications (Load · Cycling · Degradation · Post-Analysis)
| |
10-3 Feasibility Study Of
Current And Future Batteries For eVTOL Applications
|
146
|
10-3-6 Simulation Results And Comparison Of Molicel
And SiSu Cells
|
146
|
10-3-7 Conclusions
|
147
|
10-4 Fast Charging Of
High-Energy-Density LIBs For UAM
|
148
|
10-4-1 Stringent Requirements Of UAM Batteries And
The Need For A 5-Minute Ultra-Fast Charging Strategy
|
148
|
10-4-2 Definition Of UAM Mission Protocols And
Introduction Of Asymmetric Temperature Modulation (ATM)
|
149
|
10-4-3 Experimental Validation Of The ATM Method:
Prevention Of Lithium Plating And Achievement Of Ultra-Long Life
|
150
|
10-4-4 Analysis Of Lithium Plating Mechanisms And
Expansion Of The SOC Window Through Electrochemical-Thermal Modeling
|
151
|
10-4-5 Battery Performance Enhancement And
End-Of-Life (EOL) Performance Retention
|
152
|
10-5 NASA SABERS Program
|
153
|
10-5-1 SABERS Concept
|
153
|
10-5-2 Pack Energy Density
|
154
|
10-5-3 Dry Compressible Holey Graphene (hG)
|
155
|
10-5-4 All-Solid-State Composite Sulfur Cathodes And
Optimization
|
156
|
10-5-5 Holey Graphene Vs. Carbon Black And Bipolar
Stack Pouch Cells
|
157
|
|
|
11. Next-Generation Battery Development Trends: Li-Metal · All-Solid-State ·
Semi-Solid-State · Li-S ·
Hi-Ni · Bipolar Batteries
| |
11-12-4 Development Status Of WeLion
|
189
|
11-12-5 Development Status Of Qingtao Energy
|
190
|
11-12-6 Development Status Of CATL
|
191
|
11-12-7 GREPOW NCM Batteries
|
192
|
11-12-8 GREPOW NCM 5C-Rate Batteries
|
193
|
11-12-9 GREPOW High-Energy-Density Batteries
|
194
|
11-13 Bipolar Batteries
|
195
|
11-13-1 Development Trends For UAM · UAV · Drone Applications
|
195
|
11-13-2 Development History
|
196
|
11-13-3 Key Advantages And Development Status
|
197
|
11-13-4 Development Status Of TOYOTA
|
198
|
|
|
12. Fuel Cell–Based
Aircraft And UAVs (Hydrogen FC)
|
|
12-1 Fuel Cell Applications
|
200
|
12-1-1 Global Development Trends For Manned Aircraft
|
200
|
12-1-2 Development Trends For UAV And Drone
Applications
|
201
|
12-1-3 Overview Of Application Areas
|
202
|
12-1-4 Aviation And Aerospace Overview
(Systems/Propulsion, Safety And Standards)
|
203
|
12-1-5 Civil Aviation Demonstration And Roadmap,
Hybrid Integration
|
204
|
12-1-6 UAV Development History And Performance
Optimization
|
205
|
12-1-7 UAV Stack Design And Aircraft APU
Hybridization
|
206
|
12-2 Hydrogen Fuel Cell UAVs
|
207
|
12-2-1 Analysis Of Flight Profiles And Power Demand
Models
|
207
|
12-2-2 Necessity And Energy Density–Based Advantage Analysis
|
208
|
12-2-3 Impact Of Altitude Changes On UAV Power
Demand And Maximum Flight Altitude
|
209
|
12-2-4 Impact Of Altitude Changes On Fuel Cell
Thermal/Water Management And Associated Challenges
|
210
|
12-2-5 Sensitivity Analysis And Optimization
Directions For Performance Improvement
|
211
|
|
|
13. eVTOL Commercial Service Use Cases (Public Services · Logistics · Safety)
| |
13-1 eVTOL Public Services
|
212
|
13-1-1 Fighting Wildfires
|
212
|
13-1-2 Logistics Transportation During Natural
Disasters
|
213
|
13-1-3 Emergency Medical Transport
|
214
|
13-1-4 Public Safety And Law Enforcement
|
215
|
13-1-5 Last-Mile Aerial Delivery
|
216
|
|
|
14. eVTOL Company And Technology Competitive Analysis
|
|
14-1 Comparison Of
Technological Competitiveness Among The Top 6 eVTOL Companies
|
217
|
14-2 Comparison Of
Technological Competitiveness Among The Top 6 UAV (Drone) Companies
|
218
|
14-3 eVTOL Battery
Requirements Vs. GREPOW Battery Characteristics
|
219
|
14-4 Joby Aviation:
Technology And Business Strategy
|
220
|
14-5 EHang: Technology And
Commercialization Strategy
|
221
|
14-6 Comparative Patent
Analysis: Joby Vs. EHang
|
222
|
14-7 Lilium Vs. Eve:
Comparison Of Component Supplier Supply Chains
|
223
|
|
|
15. Company Trends Related To UAM-UAV (Drone)
|
|
15-21 Aridge (CN)
|
303
|
15-22 GAC (GOVY Technology)
(CN)
|
307
|
15-23 AutoFlight (CN)
|
311
|
15-24 PLANA (KR)
|
315
|
15-25 Airbility (KR)
|
319
|
15-26 SkyDrive (JP)
|
323
|
15-27 WSP (JP)
|
328
|
15-28 NASA
|
332
|
15-29 SES AI (US)
|
334
|
15-30 Development Status Of
Major Korean UAM-UAV (Drone) Companies / Consortia
|
335
|
|
|
16. Market Outlook Related To UAM-UAV (Drone)
|
|
16-1 UAM And Battery Market
Outlook
|
338
|
16-2 UAM Market Outlook
|
339
|
16-2-1 Global UAM/eVTOL Market Outlook
|
339
|
16-2-2 UAM/VTOL Technology And Market Growth
|
340
|
16-2-3 Scenario Assumptions
|
341
|
16-2-4 Regional UAM/eVTOL Market Outlook
|
342
|
16-2-5 UAM Application Battery Market Outlook
|
343
|
16-2-6 Investment Cost And Payback Potential (1)
|
344
|
16-2-7 Investment Cost And Payback Potential (2)
|
345
|
16-2-8 Domestic Status And Outlook – Government Level
|
346
|
16-2-9 Domestic Status And Outlook – Private Sector
|
347
|
16-2-10 Outlook For Domestic UAM Market Size
|
348
|
16-2-11 Domestic Status And Outlook – Operational Profitability
|
349
|
16-3 Market Size Of eVTOL
Transportation And Battery-Related Markets In China
|
350
|
16-4 Global UAV (Drone)
Market Outlook
|
351
|
16-4-1 Total Market
|
351
|
16-4-2 Military / Commercial
|
352
|
16-4-3 Market By Company
|
353
|
16-5 Global Drone Overall
Market Outlook
|
354
|
16-6 Global UAV Battery
Market Outlook
|
355
|
16-7 Global UAV (Drone)
Battery Market And Share By Battery Type
|
356
|
16-8 Major Players In The
Global UAV (Drone) Battery Market
|
357
|
|
|