Noun:

চালক যন্ত্ৰ,

bipropellant শব্দের বাংলা অর্থ এর উদাহরণ:

প্যারাসুট, অপটিক ইলেক্ট্রনিক্স, রাসায়নিক, পোশাক, আর্টিলারি, গোলাবারুদ, চালক যন্ত্ৰ, বিস্ফোরক আয় "৩.৫ বিলিয়ন (₹২৩,৬৮৭.২২ কোটি) (২০১৭–'১৮) কর্মীসংখ্যা ~৮৪ ।

কিলোগ্রাম (১,৯৬০ পা) সামগ্রিক উচ্চতা: ৪৪.৪ মিটার (১৪৫.৭ ফু) প্রপেল্যান্ট বা চালক যন্ত্ৰ: পর্যায় ১:" সংমিশ্রিত কঠিন পর্যায় ২: আর্থ স্ট্যাভেটাল তরল পর্যায় ৩: ।

bipropellant's Usage Examples:

can be monopropellant rockets using a single type of propellant, or bipropellant rockets using two types of propellant.

chemical (a monopropellant) or a mix of two chemicals, called bipropellants.

It is used as a rocket propellant in bipropellant rocket engines because it is “hypergolic” with various oxidizers such.

lower thrust and efficiency compared to conventional monopropellant and bipropellant rocket engines.

there is not one universally used propulsion system: monopropellant, bipropellant, ion propulsion, etc.

conventional coaxial distributed-element injectors typically used on liquid bipropellant rocket engines.

a rocket that uses three propellants, as opposed to the more common bipropellant rocket or monopropellant rocket designs, which use two or one propellants.

The gas-generator cycle is a power cycle of a bipropellant rocket engine.

It is a bipropellant design, using LH2 and LOX.

The combustion tap-off cycle is a power cycle of a bipropellant rocket engine.

The electric-pump-fed engine is a bipropellant rocket engine in which the fuel pumps are electrically powered, and so all of the input propellant is directly.

Dual mode propulsion systems combine the high efficiency of bipropellant rockets with the reliability and simplicity of monopropellant rockets.

as the Skylab was originally planned to be built "wet" from the spent bipropellant tanks of the Saturn S-IVB upper stage.

The Viking rocket engines were members of a series of bipropellant engines for the first and second stages of the Ariane 1 through Ariane 4 commercial.

дви́гатель 270, Rocket Engine 270, 8D420) was a single-chamber liquid-bipropellant rocket engine designed by Energomash (USSR) in 1960–1970.

contact with various forms of hydrazine, which has made the pair a common bipropellant for rockets.

for a self-igniting bipropellant combination invented to fuel its small lunar landers.

Unlike the traditional NTO/MMH bipropellant, the two propellant.

three-axis stabilized communications satellite in geostationary orbit with a bipropellant rocket propulsion system.

C-Stoff ("substance C") was a reductant used in bipropellant rocket fuels (as a fuel itself) developed by Hellmuth Walter Kommanditgesellschaft in Germany.

According to Moog-ISP, the DS2000 platform uses its bipropellant thrusters.