Rolls-Royce

BR700

Business Aviation In Production

Technical Specifications

Thrust
69.0 kN (15,500 lbf)
Bypass Ratio
4.2:1
Fan Diameter
1.270 m
Pressure Ratio
28.0:1
SFC
0.3400 lb/lbf·h
Dry Weight
1,670 kg
Length
3.240 m
First Run
1994
In Service
1996

Overview

The Rolls-Royce BR700 is a family of medium-to-large thrust turbofan engines that forms the technological foundation of Rolls-Royce's business aviation strategy. Spanning thrust ratings from approximately 13,000 lbf to 17,000 lbf across its BR710 and BR725 variants, the BR700 family powers some of the most prestigious and high-performance business jets in existence, including the Gulfstream G550 and G650, and the Bombardier Global Express series. The engine represents Rolls-Royce's commitment to competing in the large business jet segment with technology derived from its commercial aviation heritage.

The BR700 design draws on technology from Rolls-Royce's commercial RB211 and Trent families, scaled appropriately for the business jet thrust class. The engine features a three-shaft architecture — Rolls-Royce's traditional approach pioneered on the RB211 — which provides inherent aerodynamic advantages through optimized spool speeds at each compression stage. This architecture, unusual among business jet engines (most of which use two-spool designs), contributes to the BR700's high pressure ratio and competitive fuel efficiency. The FADEC system integrates engine management with aircraft avionics on the platforms it powers.

The BR700's reputation for reliability and performance in ultra-long-range business aviation has made Rolls-Royce a preferred supplier for Gulfstream and Bombardier's flagship products, the two dominant competitors in the large-cabin business jet market.

Technical Specifications

ParameterValue
Maximum Thrust69.0 kN (15,500 lbf)
Bypass Ratio4.2:1
Fan Diameter1.270 m (50.0 in)
Dry Weight1,670 kg (3,682 lb)
Length3.240 m (127.6 in)
Overall Pressure Ratio28.0:1
SFC0.340 lb/lbf·h
First Run1994
Entry into Service1996

Variants

The BR700 family comprises two major variants with distinct thrust ratings and applications. The BR710 (13,850–14,750 lbf) is the lower-thrust variant that powers the Gulfstream G550, G500, and Bombardier Global Express. The BR710C4-11 variant for the G550 achieves a maximum thrust of 15,385 lbf in the uprated configuration. The BR725 (16,900–17,000 lbf) is the higher-thrust development for the Gulfstream G650 and G650ER, featuring an increased fan diameter and improved core efficiency. The BR725 introduced new aerodynamic fan blade designs and advanced turbine materials to achieve the performance demanded by Gulfstream's flagship ultra-long-range aircraft. Both variants share a common maintenance philosophy and substantial hardware commonality to simplify spares management for operators flying multiple Gulfstream variants.

Aircraft Applications

The BR700 family powers Gulfstream's top two aircraft tiers. The Gulfstream G550 uses the BR710C4-11 (15,385 lbf) to achieve a range of 6,750 nautical miles — sufficient for non-stop transatlantic and transpacific routing. The Gulfstream G650/G650ER, the world's fastest and longest-range business jet in its category, uses the BR725A1-12 (16,900 lbf) to achieve 7,000+ nautical miles range at Mach 0.85. The Bombardier Global Express/Express XRS also uses BR710 engines. These applications at the very pinnacle of business aviation reflect the BR700's position as a premier ultra-long-range powerplant and the strength of Rolls-Royce's relationship with Gulfstream spanning multiple aircraft generations.

Development History

Rolls-Royce launched the BR700 program in the early 1990s through its BMW Rolls-Royce joint venture (the BR designation stands for BMW Rolls-Royce), established to compete in market segments not addressed by either parent company's existing lineup. The joint venture was formed in 1990, with first run of the BR710 prototype in 1994. FAA and JAA (Joint Aviation Authorities) certification was achieved in 1995–1996, with entry into service on the Bombardier Global Express in 1996. BMW's exit from the joint venture in 2000 transferred full ownership to Rolls-Royce, which rebranded the engines within its portfolio. The development of the BR725 for the Gulfstream G650 in the mid-2000s marked a significant thrust and efficiency leap, requiring new fan aerodynamics and core improvements. Rolls-Royce subsequently evolved the BR700 technology base into the Pearl family as the next-generation successor for Bombardier aircraft.