Path: utzoo!attcan!utgpu!jarvis.csri.toronto.edu!rutgers!mit-eddie!ll-xn!wjc From: wjc@XN.LL.MIT.EDU (Bill Chiarchiaro) Newsgroups: sci.space Subject: Re: Apollo Ascent Modules Summary: LM Status from NASA Message-ID: <1480@xn.LL.MIT.EDU> Date: 19 Jul 89 16:40:05 GMT References: <8907160317.AA01918@crash.cts.com> Organization: MIT Lincoln Laboratory, Lexington, MA Lines: 58 I checked the NASA Satellite Situation Report, Vol. 28, No. 4, Dec. 31, 1988 for non-booster Apollo items still in orbit. Here's what I found: Int'l Desig. Catalog # Name Orbit Mission 1969 043C 3948 LM/DESCENT Selenocentric Apollo 10 1969 043D 3949 LM/ASCENT Heliocentric Apollo 10 1969 059C 4041 LUNAR MODULE Selenocentric Apollo 11 1971 063D 5377 SUBSATELLITE Selenocentric Apollo 15 1972 031C 6005 LUNAR MODULE Selenocentric Apollo 16 The LMs from Apollos 5 (unmanned, earth-orbit test of LM-1), 9, 12, 14, 15, and 17 were all listed as decayed (actually, only the ascent stages were mentioned for 12, 14, 15, and 17). Glaringly absent, however, was any listing of the Apollo 13 LM. According to one text I have, that LM was never staged (the ascent and descent stages were kept together) and was jettisoned 18,000 km from earth. Notes on Apollo 9 and Apollo 10: As has recently been stated, Apollo 10 was the mission that was essentially a lunar dry-run of the Apollo 11 landing. We must be careful, though, in saying that its LM "descended" to within some distance of the lunar surface. Early in the mission planning, an abort from powered descent was considered, but was passed up in favor of a mission that emulated a landing in every regard except for powered descent and subsequent takeoff from the lunar surface. With Young in the CSM (Charlie Brown), Cernan and Stafford in the LM (Snoopy) performed a DOI (descent orbit insertion). This orbit had a perilune of about 15 km above the mean lunar surface -- this was their closest approach to the surface. It was from such an orbit that later LMs began their powered descents. The ascent and descent staging occured, but I don't remember at which point. Also, I believe the descent engine as well as the ascent engine was used for orbital manuevers. Cernan and Stafford spent 8 hours in the LM. Later, upon ground command, the ascent stage expended all its fuel and was put into a heliocentric orbit. One of the other forgotten Apollo mission was 9 -- the earth-orbit test of the LM. Scott stayed with the CSM (Gumdrop) and McDivitt and Schweickart spent 6 hr 20 min in the LM (Spider). They achieved a maximum separation of 185 km and did perform ascent/descent staging. Bill Chiarchiaro N1CPK wjc@xn.ll.mit.edu