Analyses on mission operations and systems for lunar landing modules are conducted. The results of the review are presented. The main subjects of the review are as follows: (1) mission operation analyses (orbits); (2) attitudes; (3) methods of detecting the barrier at landing; (4) stability at landing; (5) system configurations, weight, and power balances; (6) main propulsion system thrust and speed increments; (7) weight and electric power analyses; (8) thermal analyses; (9) communication circuits; (10) payload interfaces; (11) on-ground systems; (12) assembly methods; and (13) subsystems. Sequences up to landing on the moon are introduced as follows: (1) launch to lunar transfer orbit; (2) mid-course maneuver; (3) entry into lunar gravity range; (4) deceleration before entering lunar rotating orbit; (5) getting on the lunar rotating orbit; (6) descending maneuvering to land on the moon; (7) getting on the lunar descending orbit; (8) throttling to hovering thrust; (9) hovering at an altitude of 100 km; and (10) stopping the engine to land on the moon at an altitude of several meters.
Getsumen Chakuriku Ki No Gainen Sekkei (Conceptual Design of Lunar Landing Module)
1991
23 pages
Report
Keine Angabe
Englisch
Extraterrestrial Exploration , Lunar exploration , Lunar landing modules , Spacecraft design , Lunar landing , Space transportation system , Attitude control , Data transmission , Functional design specifications , Japanese spacecraft , Lunar probes , Lunar roving vehicles , Obstacle avoidance , Orbital maneuvers , Solar cells , Spacecraft equipment , Foreign technology
ETS-7 No Gainen Sekkei (Conceptual Study of ETS-7)
NTIS | 1992
|Tei-būmu-SSBJ-no-gainen-sekkei-ni-tsuite
TIBKAT | 2006
|Gainen sekkei tsūru-yō kūryoku tokusei dētabēsu ni tsuite
TIBKAT | 2007
|