ALMONTE WINERYBusiness Directories,Company Directories

Company Name: Corporate Name:	ALMONTE WINERY
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Company Address:	7 Houston Dr,ALMONTE,ON,Canada
ZIP Code: Postal Code:	K0A
Telephone Number:	6132566100
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USA SIC Code(Standard Industrial Classification Code):	255340
USA SIC Description:	WINEMAKING EQUIP & SUPLS
Number of Employees:	1 to 4
Sales Amount:	Less than $500,000
Credit History: Credit Report:	Unknown
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Company News:

BIT-3 RF Ion Thruster — Busek
The 56-75W input propulsion system utilizes a 2 5cm diameter grid RF ion thruster (BIT-3) and a micro RF cathode (BRFC-1) as the neutralizer The thruster’s unprecedented performance produces thrust up to 1 1 mN and specific impulse up to 2,150 seconds
Flight Development of Iodine BIT-3 RF Ion Propulsion System for SLS EM . . .
The BIT-3 ion thruster's ability to use iodine as propellant is a huge game-changer for CubeSats, as iodine is stored in high-density solid form (4 9g cc vs xenon's 1 95g cc at 2000psi) devoid of bulky pressure vessels
Flight Development of Iodine BIT-3 RF Ion Propulsion System . . . - Cal Poly
95% efficient drain voltage regulator, the RF amp would have an overall efficiency of 90% (bus voltage in → stable RF power out), a remarkable result! BIT-3 system operates at 55-75W draw and can provide >2km s deltaV to a 6U 14kg CubeSats; let’s think about taking CubeSats to Mars, Europa or asteroids!
Preparation of Papers for AIAA Technical Conferences
Abstract: A mission-enabling, iodine-fueled mini RF ion thruster was developed for CubeSat applications The thruster, designated as BIT-3 for its 3cm diameter grids, is capable of delivering variable Isp and thrust of 3200sec and 1 35mN respectively at the designed power of 60W
Busek Propulsion Systems - NASA
BIT-3 flight hardware undergoing final preparation for delivery; presently booking orders for 12 month delivery Multiple deliveries of complete integrated systems; thrusters, cathodes, PPUs, feed systems tank, harness, brackets; system hot-fire acceptance tests
The First All-Iodine Electric Propulsion Systems Launched by Busek . . .
The BIT-3 iodine thruster system is capable of generating up to two kilometers per second (4,474 m p h ) of delta-v for cubesats, opening the possibility for small spacecraft to complete a range of missions previously reserved for large, high-cost satellites
Optimizing the Design Geometry of Radio-Frequency Ion Thrusters and Ion . . .
The optimization criterion can be the thrust T for the ion thrusters or the ion current \ ( { {I}_ {0}}\) for technological ion sources calculated from the ne and Te distributions
Plasma_and_Ion_Propulsion_and_Electrospray_RCS_BCI_0525p - NASA
BIT-3 is a compact, CubeSat friendly electric propulsion system using solid iodine as propellant The system centers on a 2 5cm gridded ion engine using RF discharge
All-Electric CubeSat Propulsion Technologies
Busek BIT-3 RF Ion Thruster Performance Adaption of Iodine Technology by Busek’s Mini RF Ion Thrusters (Engines) Iodine stored as a solid low pressure, high density propellant storage The BIT series thrusters (1-7cm sized) are inherently iodine compatible The 3cm BIT-3 thruster is the world’s first gridded ion thruster using iodine
Maturation of Iodine Fueled BIT-3 RF Ion Thruster and RF Neutralizer
Maturation of Iodine Fueled BIT-3 RF Ion Thruster and RF Neutralizer