TRMM & Orihime/Hikoboshi

Launch Success

Liftoff Time (GMT)

21:27:00

Thursday November 27, 1997

Mission Details

TRMM

Wiki

TRMM (Tropical Rainfall Measuring Mission) is the first space mission dedicated to quantitatively measuring tropical and subtropical rainfall which is one of the most important and least-known parameters affecting the global climate system. TRMM is a joint project between Japan and the United States in 1986. The National Space Development Agency of Japan (NASDA) is responsible for developing a key instrument, the Precipitation Radar (PR), in collaboration with the Communications Research Laboratory (CRL) of Ministry of Public Management, Home Affairs, Posts and Telecommunications.

Low Earth Orbit

1 Payload

3,620 kilograms

Orihime/Hikoboshi

Wiki

ETS-VII (Engineering Test Satellite, "Kiku 7") was launched aboard the H-2 No. 6 rocket from Tanegashima Space Center in November 1997. ETS-VII itself comprises two satellites: "Orihime" and "Hikoboshi". "Orihime" is a target satellite weighing approximately 400 kilograms. It is placed in a fixed circular orbit at an altitude of roughly 550 kilometers. "Hikoboshi" is a chaser satellite, weighing some 2.5 tons. It moves in a variable orbit to rendezvous and dock with "Orihime". "Hikoboshi" is equipped with a six-jointed, three-clawed robot arm two meters long. Following launch of the "Orihime - Hikoboshi" satellite pair, a malfunction in the spacecraft attitude control system occurred, as well as a drop in output of the high gain antenna communication link necessary for satellite remote control. Nevertheless, the first rendezvous and docking experiment was successfully accomplished on July 7, 1998. Lessons learned from the automatic rendezvous and docking experiment entailing two unmanned satellites, and the space robotics testing involving the robot arm, are expected to contribute greatly to future space development efforts. ETS 7 reentered on 13 November 2015.

Low Earth Orbit

2 Payloads

2,860 kilograms

Rocket

Retired
H-II

Active 1994 to 1998

Mitsubishi Heavy Industries logo

Agency

MHI

Rocket

Height: 49m

Payload to Orbit

LEO: 10,060 kg

GTO: 3,930 kg

Stages

2

Strap-ons

2

Launch Site

LA-Y1

Tanegashima Space Center, Japan

Fastest Turnaround

25 days 4 hours

Stats

H-II


5th

Mission

1st

Mission of 1997

1997


77th

Orbital launch attempt