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RM

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Discoverer 19 Credit: Manufacturer Image

AKA: Radiation Meteoroid. Status: Operational 1968. First Launch: 1968-08-16. Last Launch: 1970-11-09. Number: 2 . Gross mass: 46 kg (101 lb).

SE-5-2/-3 Rocketdyne N2O4/UDMH rocket engine. SE-5-2/-3. Agena Auxiliary. Pressure-fed. SE-5-2 four engines in satellite system. SE-5-3 two engines for Agena auxiliary propulsion. First flight 1963.

P4-1 Sustainer Rocketdyne LOx/Kerosene rocket engine. AQM-37. Target System Sustainer. Pressure-fed. First flight 1963.

SE-7-85 Rocketdyne N2O4/MMH rocket engine. Gemini Orbit Attitude and Maneuvering System (85 lb thrust). Pressure-fed. First flight 1964.

SE-7-25 Rocketdyne N2O4/MMH rocket engine. Gemini Orbit Attitude and Maneuvering System (25 lb thrust). Pressure-fed. First flight 1964.

P4-1 Booster Rocketdyne LOx/Kerosene rocket engine. AQM-37. Target System Booster. Pressure-fed. First flight 1963.

SE-7-100 Rocketdyne N2O4/MMH rocket engine. Gemini Orbit Attitude and Maneuvering System (100 lb thrust). Pressure-fed. First flight 1964.

SE-6 Rocketdyne N2O4/MMH rocket engine. Gemini Re-entry Control System. Pressure-fed. First flight 1964.

SE-9-5 Rocketdyne N2O4/Aerozine-50 rocket engine. Titan III Transtage. Pressure-fed. System included two modules of three engines plus two additional SE-9-5 separate engines, tanks, and a pressurization system. First flight 1964.

SE-8 Rocketdyne N2O4/MMH rocket engine. Apollo Command Module Reaction Control. Pressure-fed. First flight 1966.

SE-9-3 Rocketdyne N2O4/Aerozine-50 rocket engine. Titan III Transtage. Pressure-fed. System included two modules of three engines plus two additional SE-9-5 separate engines, tanks, and a pressurization system. First flight 1964.

SE-7-1 Rocketdyne N2O4/MMH rocket engine. S-IVB Stage APS Ullage Control Engine (propellant settling). Pressure-fed. First flight 1966.

RS-1402 Rocketdyne N2O4/MMH rocket engine. Minuteman Pitch, Yaw & Roll Control. Pressure-fed. Technology engine, developed, but not produced. Led to RS-14 production engines.

RS-14 Rocketdyne N2O4/MMH rocket engine. Minuteman Postboost Velocity Control. Pressure-fed. First flight 1970.

RS-1403 Rocketdyne N2O4/MMH rocket engine. Minuteman Pitch, Yaw & Roll Control. Pressure-fed. Technology engine, developed, but not produced. Led to RS-14 production engines.

RM-05 Rocketdyne N2O4/MMH rocket engine. Satellite Reaction Control System. Pressure-fed.

RM-1-1 Rocketdyne N2O4/MMH rocket engine. Satellite Reaction Control System. Pressure-fed.

RM-1-2 Rocketdyne N2O4/MMH rocket engine. Satellite Reaction Control. Pressure-fed.

RM-100B Rocketdyne Nitric acid/UDMH rocket engine. Satellite Reaction Control. Pressure-fed.

RM-100T Rocketdyne N2O4/Aerozine-50 rocket engine. Lunar Flyer. Pressure-fed.

RM-25 Rocketdyne N2O4/MMH rocket engine. Spacecraft. Pressure-fed.

RM-100A Rocketdyne N2O4/MMH rocket engine. Spacecraft. Pressure-fed.

RM-25-1 Rocketdyne N2O4/MMH rocket engine. Spacecraft. Pressure-fed.

RS-2101C Rocketdyne N2O4/MMH rocket engine. Viking. Pressure-fed. Derivative of RS-14 Minuteman engine. First flight 1975.

RS-2101A Rocketdyne N2O4/MMH rocket engine. Mars Mariner. Pressure-fed. Derivative of RS-14 Minuteman engine. First flight 1971.

RESA-2 Rocketdyne N2O4/MMH rocket engine. Pitch Control Propulsion Module. Pressure-fed.

RESA-5 Rocketdyne N2O4/MMH rocket engine. Spacecraft. Pressure-fed.

RM-1500H Rocketdyne LOx/LH2 rocket engine. Space Shuttle Orbiter Auxiliary Propulsion. Pressure-fed.

RM-900 Rocketdyne N2O4/MMH rocket engine. Shuttle Orbiter Reaction Control. Pressure-fed.

RS-28 Rocketdyne N2O4/MMH rocket engine. Space Shuttle Orbiter Reaction Control. Pressure-fed.

RS-32 Rocketdyne N2O4/MMH rocket engine. Upper Stage Target Engine Systems. Pressure-fed. Derived from Minuteman RS-14.

RS-34 Attitude Control Rocketdyne LOx/Kerosene rocket engine. Peacekeeper Postboost Attitude Control. Pressure-fed. 8 attitude thrusters in each postboost propulsion system. First flight 1983.

RS-36 Sustainer Rocketdyne LOx/Kerosene rocket engine. HOE Homing Overlay Experiment Upper Stage Axial Propulsion System. Pressure-fed. Derivative of Lance propulsion system. First flight 1983.

RS-43 Rocketdyne N2O4/MMH rocket engine. Attitude Control. Pressure-fed.

RS-42 Rocketdyne N2O4/MMH rocket engine. Axial Spacecraft. Pressure-fed.

RS-45 Rocketdyne N2O4/MMH rocket engine. Satellite Attitude Control and Stationkeeping. Pressure-fed.

KEW-1 Rocketdyne N2O4/MMH rocket engine. Kinetic Energy Propulsion (7 lb thrust). Pressure-fed. ASAT Strap-down test, XSS / DICE Microsatellite, GBI Ground-Based Interceptor, THAAD Theater High Altitude Area Defense.

KEW-3 Rocketdyne N2O4/MMH rocket engine. Kinetic Energy Propulsion (100 lb thrust). Pressure-fed. ASAT Strap-down test, XSS / DICE Microsatellite, GBI Ground-Based Interceptor, THAAD Theater High Altitude Area Defense.

KEW-2 Rocketdyne N2O4/MMH rocket engine. Kinetic Energy Propulsion (50 lb thrust). Pressure-fed. ASAT Strap-down test, XSS / DICE Microsatellite, GBI Ground-Based Interceptor, THAAD Theater High Altitude Area Defense.

KEW-4 Rocketdyne N2O4/MMH rocket engine. Kinetic Energy Propulsion (500 lb thrust). Pressure-fed. ASAT Strap-down test, XSS / DICE Microsatellite, GBI Ground-Based Interceptor, THAAD Theater High Altitude Area Defense.

Photo Gallery

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RM-1; RMS Credit: Manufacturer Image

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RM 1 Credit: Manufacturer Image

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RM-18 Credit: Manufacturer Image

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• RM-18 - . Payload: RM-18. Mass: 46 kg (101 lb). Nation: USA. Agency: USAF AFSC. Spacecraft: RM.

• RM-1; RMS - . Payload: RM/FW4S. Mass: 46 kg (101 lb). Nation: USA. Agency: NASA Houston. Class: Earth. Type: Micrometeoroid satellite. Spacecraft: RM. Decay Date: 1971-02-07 . USAF Sat Cat: 4692 . COSPAR: 1970-094B. Apogee: 526 km (326 mi). Perigee: 303 km (188 mi). Inclination: 37.40 deg. Period: 92.70 min. Radiation Meteoroid. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .