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RM
Discoverer 19
Discoverer 19
Credit: Manufacturer Image
American earth micrometeoroid satellite. Spacecraft engaged in research and exploration of the upper atmosphere or outer space. Research, meteoroids and radiation satellite operated by NASA, USA. Launched 1970. Used the Scout-B stage 4 bus.

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


More at: RM.

Subtopics

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.

Family: Earth, Earth micrometeoroid sat. Country: USA. Launch Vehicles: Atlas, Scout, Atlas F, Scout B, Atlas Burner 2. Launch Sites: Wallops Island, Vandenberg, Vandenberg SLC3E, Wallops Island LA3A. Agency: NASA. Bibliography: 2, 279, 6, 11695.
Photo Gallery

RM-1; RMSRM-1; RMS
Credit: Manufacturer Image


RM 1RM 1
Credit: Manufacturer Image


RM-18RM-18
Credit: Manufacturer Image



1968 August 16 - . 20:57 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas Burner 2. FAILURE: Failure.
  • RM-18 - . Payload: RM-18. Mass: 46 kg (101 lb). Nation: USA. Agency: USAF AFSC. Spacecraft: RM.

1970 November 9 - . 06:00 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA3A. LV Family: Scout. Launch Vehicle: Scout B.
  • 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: 37.4000 deg. Period: 92.70 min. Radiation Meteoroid. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .


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