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11D428A-16 (製造社名RDMT-135M)はN2O4/UDMHをO/F1. … 11D428A-16 (製造社名RDMT-135M)はN2O4/UDMHをO/F1.85で燃焼する液体加圧供給式ロケットエンジンである。有人仕様の宇宙機の推進方法用途で使用される。現在は宇宙船推進モジュールで使用される。以前の派生型である11D428A (製造者名RDMT-135) は現在もズヴェスダISSモジュールの姿勢制御システムとして使用される。11D428A-16は129.16 N (29.04 lbf)の推力を生み出し、燃焼室圧力は0.88 MPa (128 psi)で比推力は291秒 (2.85 km/s)に到達する。500,000回の始動と燃焼時間は0.03秒から2000秒である。それぞれのユニットの重量は1.5 kg (3.3 lb)である。ら2000秒である。それぞれのユニットの重量は1.5 kg (3.3 lb)である。
, The 11D428A-16 (manufacturer's name RDMT-1 … The 11D428A-16 (manufacturer's name RDMT-135M) is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated spacecraft propulsion applications. It is currently used in the KTDU-80 spacecraft propulsion module. The previous version, the 11D428A (manufacturer's name RDMT-135) is still used as the reaction control system thrusters of the Zvezda ISS module.The 11D428A-16 generates 129.16 N (29.04 lbf) of thrust with a chamber pressure of 0.88 MPa (128 psi) and achieves a specific impulse of 291 s (2.85 km/s). It is rated for 500,000 starts with a certified ignition time of 0.03 seconds to 2000 seconds. Each unit weights 1.5 kg (3.3 lb).econds. Each unit weights 1.5 kg (3.3 lb).
, O 11D428 (também conhecido como RDMT-135M), é um motor de foguete a combustível líquido queimando N2O4/UDMH. Ele é usado para efetuar manobras em espaçonaves tripuladas, fazendo parte do módulo de propulsão KTDU-80.
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| rdfs:comment |
11D428A-16 (製造社名RDMT-135M)はN2O4/UDMHをO/F1. … 11D428A-16 (製造社名RDMT-135M)はN2O4/UDMHをO/F1.85で燃焼する液体加圧供給式ロケットエンジンである。有人仕様の宇宙機の推進方法用途で使用される。現在は宇宙船推進モジュールで使用される。以前の派生型である11D428A (製造者名RDMT-135) は現在もズヴェスダISSモジュールの姿勢制御システムとして使用される。11D428A-16は129.16 N (29.04 lbf)の推力を生み出し、燃焼室圧力は0.88 MPa (128 psi)で比推力は291秒 (2.85 km/s)に到達する。500,000回の始動と燃焼時間は0.03秒から2000秒である。それぞれのユニットの重量は1.5 kg (3.3 lb)である。ら2000秒である。それぞれのユニットの重量は1.5 kg (3.3 lb)である。
, O 11D428 (também conhecido como RDMT-135M), é um motor de foguete a combustível líquido queimando N2O4/UDMH. Ele é usado para efetuar manobras em espaçonaves tripuladas, fazendo parte do módulo de propulsão KTDU-80.
, The 11D428A-16 (manufacturer's name RDMT-1 … The 11D428A-16 (manufacturer's name RDMT-135M) is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated spacecraft propulsion applications. It is currently used in the KTDU-80 spacecraft propulsion module. The previous version, the 11D428A (manufacturer's name RDMT-135) is still used as the reaction control system thrusters of the Zvezda ISS module.The 11D428A-16 generates 129.16 N (29.04 lbf) of thrust with a chamber pressure of 0.88 MPa (128 psi) and achieves a specific impulse of 291 s (2.85 km/s). It is rated for 500,000 starts with a certified ignition time of 0.03 seconds to 2000 seconds. Each unit weights 1.5 kg (3.3 lb).econds. Each unit weights 1.5 kg (3.3 lb).
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| rdfs:label |
11D428
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