IAR 111
# IAR 111

The IAR-111 Excelsior was a supersonic mothership project, designed by ARCA Space Corporation, intended to transport a rocket payload up to 18,000 m (59,000 ft) and for developing space tourism related technologies. The aircraft was supposed to be constructed almost entirely from composite materials, and was to be designed for take-off and landing from the sea surface.

The project has since been abandoned.

## History

The design of the aircraft started before the successful launch of the Helen 2 rocket. ARCA kept work on the project secret and decided to reveal it to the public in a press conference that took place at BRD headquarters in Bucharest in December 2010. The initial name of the aircraft was E-111. In March 2011 ARCA received approval from IAR S.A. Brasov to use its initials on the aircraft, so E-111 was officially renamed IAR-111.

Work on the fuselage moulds started in early 2011 and were completed in September. The cockpit structure was completed in July. It is detachable from the rest of the aircraft and will be equipped with two rocket propelled parachutes (main and back-up) as a safety system. Also in September the CFD simulations for the aircraft were completed. On 29 September 2011, a successful cockpit drop-test was carried out. A Mi-17 helicopter dropped the cockpit from 700 m (2,300 ft) to test the parachute recovery system. In December 2011, the first two sections of the aircraft fuselage were completed and preliminary assembled.

## Design

### Features

The IAR-111 is designed to take-off and land on the sea surface. ARCA decided to use this approach to eliminate the need for a landing gear and thus reduce the cost of the aircraft. Another factor that went into the decision was the fact that Romania has no unpopulated areas above which to safely test the aircraft to high altitude flights.

The aircraft has diamond-shaped wings to reduce weight, and lower drag at high speeds; "V" tails were chosen to avoid contact with the water on take-off and landing. It has two floats and the payload is located between them, acting as a third float. The payload will be either the Haas 2 rocket or an external fuel tank.

For aerodynamic surface control it will use a hydraulic system controlled by fly-by-wire from the cockpit. The aircraft will be powered by the new Executor liquid-fuelled rocket engine, under construction at ARCA, which will use kerosene as fuel and liquid oxygen as oxidizer.

### Safety

The cockpit walls and windows are very thick, able to withstand an engine explosion in case of failure of the rocket. Additionally, the cockpit is detachable and is equipped with two rocket propelled parachutes (main and back-up). The aircraft will have a very large recovery parachute and a smaller anti-stall parachute.

Mission 6 tested the safety systems with a drop test from 700 m (2,300 ft). One of the parachutes was opened to test the explosive bolts. The test was a success and the cabin was recovered in good condition.

## Specifications

The specifications released to date are approximate design goals, and include:

Data from ARCA

General characteristics

* Crew: 2
* Length: 24 m (78 ft 9 in)
* Wingspan: 12 m (39 ft 4 in)
* Height: 5 m (16 ft 5 in)
* Wing area: 100 $m^2$ (1,100 sq ft)
* Empty weight: 7,200 kg (15,873 lb)
* Gross weight: 19,000 kg (41,888 lb)
* Max takeoff weight: 23,000 kg (50,706 lb)
* Powerplant: 1 × Executor liquid-fuelled rocket engine, 200 kN (44,000 lbf) thrust

Performance

* Maximum speed: Mach 2.6
* Service ceiling: 100,000 m (330,000 ft)
* Rate of climb: 250 m/s (49,000 ft/min)
* Wing loading: 230 $kg/m^2$ (47 lb/sq ft)
* Thrust/weight: 2.316
