GB/T 42856-2023Flight test requirements for civil large and medium unmanned helicopter systems flight performance (English PDF)
民用大中型无人直升机系统飞行性能飞行试验要求
This is a limited preview
Buy now to download the full PDF (15 pages)
Need quotation for your management?
Get a formal quotation for GB/T 42856-2023 in 30 minutes.
Issued by
SAMR; SAC
Level / Type
National · Recommended
Issue date
August 6, 2023
Implementation date
March 1, 2024
Scope
GB/T 42856-2023 is the English-translated version of 民用大中型无人直升机系统飞行性能飞行试验要求.
This document specifies the flight testing of the flight performance of large and medium civil unmanned helicopter systems: what the test covers, its purpose, the conditions it requires, how it is carried out, how the data are processed and how the result is evaluated.
The document applies to the performance flight testing of civil unmanned helicopter systems with a maximum take-off mass of not less than 150 kg powered by fuel or by batteries; the flight testing of unmanned helicopters of other types may follow it as a reference.
Found what you need?
Document preview — GB/T 42856-2023
National Standard of the People's Republic of China
- ICS
- 49.060
- Classification
- V 37
Issued by: State Administration for Market Regulation; Standardization Administration of the PRC
Contents
- PrefaceI
- 1 Scope
- 2 Normative reference documents
- 3 Terms and Definitions
- 4 General requirements
- 4.1 Test flight conditions
- 4.2 Test flight object
- 4.3 Test flight testing and test modification
- 4.4 Test flight data processing
- 5 Detailed requirements
- 5.1 Static pressure and airspeed measurement system calibration
- 5.2 Engine installed power loss
- 5.3 Take off
- 5.4 Inclined climb
- 5.5 Rotation
- 5.6 Hovering and Vertical Climb
- 5.7 Landing
- 5.8 Level flight
- 5.9 Limit height-speed envelope
- 5.10 Do not exceed speed
- 5.11 Battery life
- 6 Test flight report
Foreword
This document complies with the provisions of GB/T 1.1-2020 "Standardization Work Guidelines Part 1: Structure and Drafting Rules of Standardization Documents" Drafting.
1 Scope
This document specifies the content, purpose, conditions, implementation, data processing and Result evaluation and other requirements.
This document is applicable to civil unmanned helicopter systems with a maximum take-off weight of not less than 150kg and using fuel or batteries as power source.
Performance test flight, other types of unmanned helicopter test flights can be used as a reference.
2 Normative reference documents
The contents of the following documents constitute essential provisions of this document through normative references in the text. Among them, the dated quotations For undated referenced documents, only the version corresponding to that date applies to this document; for undated referenced documents, the latest version (including all amendments) applies to this document.
GB/T 38152 Unmanned aircraft system terminology
3 Terms and definitions
The terms and definitions defined in GB/T 38152 apply to this document.
4 General requirements
4.1 Test flight conditions
The test flight site conditions (altitude, size and surface material of the runway or landing area, etc.) and atmospheric conditions (atmospheric temperature, atmospheric pressure, etc.)
Atmospheric humidity and icing, etc.) should comply with the relevant provisions in the model technical requirements.
4.2 Test flight objects
4.2.1 General
The technical status of the test flight object (the unmanned helicopter system being tested) should comply with the model technical requirements. Unless there are special provisions, the test flight objects are still Shall comply with the requirements of 4.2.2 and 4.2.3.
4.2.2 Power plant
4.2.2.1 Engine power guarantee
The performance of the installed engine should not be lower than the minimum guaranteed performance of the engine. During the test flight, the engine maintenance requirements should be followed. Perform a guaranteed power check.
4.2.2.2 Power failure
If shutting down the power unit, setting idle or using partial power is used to simulate power failure, it should be proven that the simulation method is consistent with the real power.
......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 15 pages — is available in the English PDF.
Referenced standards
Normative references
Similar standards
How to Download GB/T 42856-2023
- 1
Add to cart
Click "Download PDF" on this page and choose "Buy this standard". You can add more standards before checkout.
- 2
Checkout
Enter your email and billing details. Payment is processed securely by Stripe (cards or bank transfer). Prefer bank details? Request a quotation (min. order $300).
- 3
Instant delivery (0–9 sec)
Delivery is automatic: within seconds of payment you'll receive an email with a secure download link. The link stays valid for 72 hours.
- 4
Invoice included
A tax invoice is attached to the confirmation email. Need a custom invoice? Contact us.
Related Standards
GB/T 38152-2019 — Terminology for unmanned aircraft system
GB/T 10003-2026 — Biaxially oriented polypropylene (BOPP) film
GB/T 10004-2026 — Plastic/Plastic laminated films and pouches for packaging
Secure payment via Stripe
Payments accepted
GB/T 42856-2023
$210.00